SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
SCIENTIAM QUIA OMNES
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
AEROSPACE ENGINEERING
PROPELLANT MASTER REGISTER
PROPELLANT MASTER REGISTER
PROPELLANT MASTER REGISTER
PROPELLANT MASTER REGISTER
PROPELLANT MASTER REGISTER
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO, Nitrogen Tetroxide
NTO-Aerozine-25
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (25%) UDMH (75%)
25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
53.085’12
Mixture Ratio (X:1)
1.85
Specific Impulse (seconds @ sl)
278
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,730
Reference Velocity (exhaust m / s)
1,725
Chamber Temperature (K)
3,268
Exhaust Weight (g / mole)
21.40
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.15
| NTO-Aerozine-25 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (25%) UDMH (75%) 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 53.085’12 Mixture Ratio (X:1) 1.85 Specific Impulse (seconds @ sl) 278 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,730 Reference Velocity (exhaust m / s) 1,725 Chamber Temperature (K) 3,268 Exhaust Weight (g / mole) 21.40 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.15 |
NTO-Aerozine-25
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (25%) UDMH (75%)
25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
53.085’12
Mixture Ratio (X:1)
1.85
Specific Impulse (seconds @ sl)
278
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,730
Reference Velocity (exhaust m / s)
1,725
Chamber Temperature (K)
3,268
Exhaust Weight (g / mole)
21.40
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.15
| NTO-Aerozine-25 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (25%) UDMH (75%) 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 53.085’12 Mixture Ratio (X:1) 1.85 Specific Impulse (seconds @ sl) 278 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,730 Reference Velocity (exhaust m / s) 1,725 Chamber Temperature (K) 3,268 Exhaust Weight (g / mole) 21.40 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.15 |
NTO-Aerozine-25
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (25%) UDMH (75%)
25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
53.085’12
Mixture Ratio (X:1)
1.85
Specific Impulse (seconds @ sl)
278
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,730
Reference Velocity (exhaust m / s)
1,725
Chamber Temperature (K)
3,268
Exhaust Weight (g / mole)
21.40
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.15
| NTO-Aerozine-25 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (25%) UDMH (75%) 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 53.085’12 Mixture Ratio (X:1) 1.85 Specific Impulse (seconds @ sl) 278 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,730 Reference Velocity (exhaust m / s) 1,725 Chamber Temperature (K) 3,268 Exhaust Weight (g / mole) 21.40 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.15 |
NTO-Aerozine-25
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (25%) UDMH (75%)
25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
53.085’12
Mixture Ratio (X:1)
1.85
Specific Impulse (seconds @ sl)
278
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,730
Reference Velocity (exhaust m / s)
1,725
Chamber Temperature (K)
3,268
Exhaust Weight (g / mole)
21.40
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.15
| NTO-Aerozine-25 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (25%) UDMH (75%) 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 53.085’12 Mixture Ratio (X:1) 1.85 Specific Impulse (seconds @ sl) 278 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,730 Reference Velocity (exhaust m / s) 1,725 Chamber Temperature (K) 3,268 Exhaust Weight (g / mole) 21.40 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.15 |
NTO-Aerozine-25
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (25%) UDMH (75%)
25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
53.085’12
Mixture Ratio (X:1)
1.85
Specific Impulse (seconds @ sl)
278
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,730
Reference Velocity (exhaust m / s)
1,725
Chamber Temperature (K)
3,268
Exhaust Weight (g / mole)
21.40
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.15
| NTO-Aerozine-25 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (25%) UDMH (75%) 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 53.085’12 Mixture Ratio (X:1) 1.85 Specific Impulse (seconds @ sl) 278 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,730 Reference Velocity (exhaust m / s) 1,725 Chamber Temperature (K) 3,268 Exhaust Weight (g / mole) 21.40 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.15 |
NTO-Aerozine-50
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.59
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
326
Effective Velocity (exhaust m / s)
2,750
Reference Velocity (exhaust m / s)
1,738
Chamber Temperature (K)
3,229
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-Aerozine-50 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.59 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 326 Effective Velocity (exhaust m / s) 2,750 Reference Velocity (exhaust m / s) 1,738 Chamber Temperature (K) 3,229 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-Aerozine-50
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.59
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
326
Effective Velocity (exhaust m / s)
2,750
Reference Velocity (exhaust m / s)
1,738
Chamber Temperature (K)
3,229
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-Aerozine-50 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.59 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 326 Effective Velocity (exhaust m / s) 2,750 Reference Velocity (exhaust m / s) 1,738 Chamber Temperature (K) 3,229 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-Aerozine-50
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.59
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
326
Effective Velocity (exhaust m / s)
2,750
Reference Velocity (exhaust m / s)
1,738
Chamber Temperature (K)
3,229
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-Aerozine-50 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.59 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 326 Effective Velocity (exhaust m / s) 2,750 Reference Velocity (exhaust m / s) 1,738 Chamber Temperature (K) 3,229 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-Aerozine-50
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.59
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
326
Effective Velocity (exhaust m / s)
2,750
Reference Velocity (exhaust m / s)
1,738
Chamber Temperature (K)
3,229
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-Aerozine-50 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.59 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 326 Effective Velocity (exhaust m / s) 2,750 Reference Velocity (exhaust m / s) 1,738 Chamber Temperature (K) 3,229 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-Aerozine-50
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.59
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
326
Effective Velocity (exhaust m / s)
2,750
Reference Velocity (exhaust m / s)
1,738
Chamber Temperature (K)
3,229
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-Aerozine-50 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.59 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 326 Effective Velocity (exhaust m / s) 2,750 Reference Velocity (exhaust m / s) 1,738 Chamber Temperature (K) 3,229 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-Ammonia
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.89
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,615
Reference Velocity (exhaust m / s)
1,644
Chamber Temperature (K)
2,860
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.04
| NTO-Ammonia ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.89 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,615 Reference Velocity (exhaust m / s) 1,644 Chamber Temperature (K) 2,860 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.04 |
NTO-Ammonia
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.89
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,615
Reference Velocity (exhaust m / s)
1,644
Chamber Temperature (K)
2,860
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.04
| NTO-Ammonia ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.89 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,615 Reference Velocity (exhaust m / s) 1,644 Chamber Temperature (K) 2,860 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.04 |
NTO-Ammonia
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.89
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,615
Reference Velocity (exhaust m / s)
1,644
Chamber Temperature (K)
2,860
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.04
| NTO-Ammonia ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.89 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,615 Reference Velocity (exhaust m / s) 1,644 Chamber Temperature (K) 2,860 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.04 |
NTO-Ammonia
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.89
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,615
Reference Velocity (exhaust m / s)
1,644
Chamber Temperature (K)
2,860
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.04
| NTO-Ammonia ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.89 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,615 Reference Velocity (exhaust m / s) 1,644 Chamber Temperature (K) 2,860 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.04 |
NTO-Ammonia
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.89
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,615
Reference Velocity (exhaust m / s)
1,644
Chamber Temperature (K)
2,860
Exhaust Weight (g / mole)
20.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.04
| NTO-Ammonia ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.89 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,615 Reference Velocity (exhaust m / s) 1,644 Chamber Temperature (K) 2,860 Exhaust Weight (g / mole) 20.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.04 |
NTO-Aniline
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.64
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
336
Effective Velocity (exhaust m / s)
2,538
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,452
Exhaust Weight (g / mole)
26.00
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.30
| NTO-Aniline ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.64 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 336 Effective Velocity (exhaust m / s) 2,538 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,452 Exhaust Weight (g / mole) 26.00 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.30 |
NTO-Aniline
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.64
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
336
Effective Velocity (exhaust m / s)
2,538
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,452
Exhaust Weight (g / mole)
26.00
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.30
| NTO-Aniline ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.64 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 336 Effective Velocity (exhaust m / s) 2,538 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,452 Exhaust Weight (g / mole) 26.00 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.30 |
NTO-Aniline
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.64
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
336
Effective Velocity (exhaust m / s)
2,538
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,452
Exhaust Weight (g / mole)
26.00
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.30
| NTO-Aniline ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.64 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 336 Effective Velocity (exhaust m / s) 2,538 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,452 Exhaust Weight (g / mole) 26.00 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.30 |
NTO-Aniline
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.64
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
336
Effective Velocity (exhaust m / s)
2,538
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,452
Exhaust Weight (g / mole)
26.00
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.30
| NTO-Aniline ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.64 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 336 Effective Velocity (exhaust m / s) 2,538 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,452 Exhaust Weight (g / mole) 26.00 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.30 |
NTO-Aniline
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.64
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
336
Effective Velocity (exhaust m / s)
2,538
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,452
Exhaust Weight (g / mole)
26.00
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.30
| NTO-Aniline ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.64 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 336 Effective Velocity (exhaust m / s) 2,538 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,452 Exhaust Weight (g / mole) 26.00 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.30 |
NTO-Ethanol-75
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (75%) Water (25%)
75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
38.047’21
Mixture Ratio (X:1)
1.93
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
293
Effective Velocity (exhaust m / s)
2,479
Reference Velocity (exhaust m / s)
1,551
Chamber Temperature (K)
3,006
Exhaust Weight (g / mole)
24.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-75 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (75%) Water (25%) 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 38.047’21 Mixture Ratio (X:1) 1.93 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 293 Effective Velocity (exhaust m / s) 2,479 Reference Velocity (exhaust m / s) 1,551 Chamber Temperature (K) 3,006 Exhaust Weight (g / mole) 24.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-75
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (75%) Water (25%)
75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
38.047’21
Mixture Ratio (X:1)
1.93
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
293
Effective Velocity (exhaust m / s)
2,479
Reference Velocity (exhaust m / s)
1,551
Chamber Temperature (K)
3,006
Exhaust Weight (g / mole)
24.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-75 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (75%) Water (25%) 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 38.047’21 Mixture Ratio (X:1) 1.93 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 293 Effective Velocity (exhaust m / s) 2,479 Reference Velocity (exhaust m / s) 1,551 Chamber Temperature (K) 3,006 Exhaust Weight (g / mole) 24.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-75
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (75%) Water (25%)
75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
38.047’21
Mixture Ratio (X:1)
1.93
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
293
Effective Velocity (exhaust m / s)
2,479
Reference Velocity (exhaust m / s)
1,551
Chamber Temperature (K)
3,006
Exhaust Weight (g / mole)
24.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-75 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (75%) Water (25%) 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 38.047’21 Mixture Ratio (X:1) 1.93 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 293 Effective Velocity (exhaust m / s) 2,479 Reference Velocity (exhaust m / s) 1,551 Chamber Temperature (K) 3,006 Exhaust Weight (g / mole) 24.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-75
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (75%) Water (25%)
75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
38.047’21
Mixture Ratio (X:1)
1.93
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
293
Effective Velocity (exhaust m / s)
2,479
Reference Velocity (exhaust m / s)
1,551
Chamber Temperature (K)
3,006
Exhaust Weight (g / mole)
24.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-75 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (75%) Water (25%) 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 38.047’21 Mixture Ratio (X:1) 1.93 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 293 Effective Velocity (exhaust m / s) 2,479 Reference Velocity (exhaust m / s) 1,551 Chamber Temperature (K) 3,006 Exhaust Weight (g / mole) 24.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-75
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (75%) Water (25%)
75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
38.047’21
Mixture Ratio (X:1)
1.93
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
293
Effective Velocity (exhaust m / s)
2,479
Reference Velocity (exhaust m / s)
1,551
Chamber Temperature (K)
3,006
Exhaust Weight (g / mole)
24.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-75 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (75%) Water (25%) 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 38.047’21 Mixture Ratio (X:1) 1.93 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 293 Effective Velocity (exhaust m / s) 2,479 Reference Velocity (exhaust m / s) 1,551 Chamber Temperature (K) 3,006 Exhaust Weight (g / mole) 24.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-95
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
2.26
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,540
Reference Velocity (exhaust m / s)
1,593
Chamber Temperature (K)
3,151
Exhaust Weight (g / mole)
24.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-95 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 2.26 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,540 Reference Velocity (exhaust m / s) 1,593 Chamber Temperature (K) 3,151 Exhaust Weight (g / mole) 24.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-95
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
2.26
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,540
Reference Velocity (exhaust m / s)
1,593
Chamber Temperature (K)
3,151
Exhaust Weight (g / mole)
24.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-95 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 2.26 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,540 Reference Velocity (exhaust m / s) 1,593 Chamber Temperature (K) 3,151 Exhaust Weight (g / mole) 24.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-95
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
2.26
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,540
Reference Velocity (exhaust m / s)
1,593
Chamber Temperature (K)
3,151
Exhaust Weight (g / mole)
24.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-95 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 2.26 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,540 Reference Velocity (exhaust m / s) 1,593 Chamber Temperature (K) 3,151 Exhaust Weight (g / mole) 24.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-95
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
2.26
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,540
Reference Velocity (exhaust m / s)
1,593
Chamber Temperature (K)
3,151
Exhaust Weight (g / mole)
24.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-95 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 2.26 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,540 Reference Velocity (exhaust m / s) 1,593 Chamber Temperature (K) 3,151 Exhaust Weight (g / mole) 24.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-Ethanol-95
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
2.26
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,540
Reference Velocity (exhaust m / s)
1,593
Chamber Temperature (K)
3,151
Exhaust Weight (g / mole)
24.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.16
| NTO-Ethanol-95 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 2.26 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,540 Reference Velocity (exhaust m / s) 1,593 Chamber Temperature (K) 3,151 Exhaust Weight (g / mole) 24.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.16 |
NTO-HTPB
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
3.26
Specific Impulse (seconds @ sl)
262
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,571
Reference Velocity (exhaust m / s)
1,625
Chamber Temperature (K)
3,408
Exhaust Weight (g / mole)
25.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.28
| NTO-HTPB ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 3.26 Specific Impulse (seconds @ sl) 262 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,571 Reference Velocity (exhaust m / s) 1,625 Chamber Temperature (K) 3,408 Exhaust Weight (g / mole) 25.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.28 |
NTO-HTPB
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
3.26
Specific Impulse (seconds @ sl)
262
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,571
Reference Velocity (exhaust m / s)
1,625
Chamber Temperature (K)
3,408
Exhaust Weight (g / mole)
25.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.28
| NTO-HTPB ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 3.26 Specific Impulse (seconds @ sl) 262 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,571 Reference Velocity (exhaust m / s) 1,625 Chamber Temperature (K) 3,408 Exhaust Weight (g / mole) 25.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.28 |
NTO-HTPB
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
3.26
Specific Impulse (seconds @ sl)
262
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,571
Reference Velocity (exhaust m / s)
1,625
Chamber Temperature (K)
3,408
Exhaust Weight (g / mole)
25.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.28
| NTO-HTPB ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 3.26 Specific Impulse (seconds @ sl) 262 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,571 Reference Velocity (exhaust m / s) 1,625 Chamber Temperature (K) 3,408 Exhaust Weight (g / mole) 25.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.28 |
NTO-HTPB
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
3.26
Specific Impulse (seconds @ sl)
262
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,571
Reference Velocity (exhaust m / s)
1,625
Chamber Temperature (K)
3,408
Exhaust Weight (g / mole)
25.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.28
| NTO-HTPB ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 3.26 Specific Impulse (seconds @ sl) 262 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,571 Reference Velocity (exhaust m / s) 1,625 Chamber Temperature (K) 3,408 Exhaust Weight (g / mole) 25.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.28 |
NTO-HTPB
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
3.26
Specific Impulse (seconds @ sl)
262
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,571
Reference Velocity (exhaust m / s)
1,625
Chamber Temperature (K)
3,408
Exhaust Weight (g / mole)
25.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.28
| NTO-HTPB ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ HTPB Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 3.26 Specific Impulse (seconds @ sl) 262 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,571 Reference Velocity (exhaust m / s) 1,625 Chamber Temperature (K) 3,408 Exhaust Weight (g / mole) 25.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.28 |
NTO-Hydrazine
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.08
Specific Impulse (seconds @ sl)
286
Density Impulse (kg · s · l @ sl)
342
Effective Velocity (exhaust m / s)
2,803
Reference Velocity (exhaust m / s)
1,771
Chamber Temperature (K)
3,137
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.19
| NTO-Hydrazine ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.08 Specific Impulse (seconds @ sl) 286 Density Impulse (kg · s · l @ sl) 342 Effective Velocity (exhaust m / s) 2,803 Reference Velocity (exhaust m / s) 1,771 Chamber Temperature (K) 3,137 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.19 |
NTO-Hydrazine
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.08
Specific Impulse (seconds @ sl)
286
Density Impulse (kg · s · l @ sl)
342
Effective Velocity (exhaust m / s)
2,803
Reference Velocity (exhaust m / s)
1,771
Chamber Temperature (K)
3,137
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.19
| NTO-Hydrazine ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.08 Specific Impulse (seconds @ sl) 286 Density Impulse (kg · s · l @ sl) 342 Effective Velocity (exhaust m / s) 2,803 Reference Velocity (exhaust m / s) 1,771 Chamber Temperature (K) 3,137 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.19 |
NTO-Hydrazine
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.08
Specific Impulse (seconds @ sl)
286
Density Impulse (kg · s · l @ sl)
342
Effective Velocity (exhaust m / s)
2,803
Reference Velocity (exhaust m / s)
1,771
Chamber Temperature (K)
3,137
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.19
| NTO-Hydrazine ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.08 Specific Impulse (seconds @ sl) 286 Density Impulse (kg · s · l @ sl) 342 Effective Velocity (exhaust m / s) 2,803 Reference Velocity (exhaust m / s) 1,771 Chamber Temperature (K) 3,137 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.19 |
NTO-Hydrazine
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.08
Specific Impulse (seconds @ sl)
286
Density Impulse (kg · s · l @ sl)
342
Effective Velocity (exhaust m / s)
2,803
Reference Velocity (exhaust m / s)
1,771
Chamber Temperature (K)
3,137
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.19
| NTO-Hydrazine ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.08 Specific Impulse (seconds @ sl) 286 Density Impulse (kg · s · l @ sl) 342 Effective Velocity (exhaust m / s) 2,803 Reference Velocity (exhaust m / s) 1,771 Chamber Temperature (K) 3,137 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.19 |
NTO-Hydrazine
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.08
Specific Impulse (seconds @ sl)
286
Density Impulse (kg · s · l @ sl)
342
Effective Velocity (exhaust m / s)
2,803
Reference Velocity (exhaust m / s)
1,771
Chamber Temperature (K)
3,137
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.19
| NTO-Hydrazine ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.08 Specific Impulse (seconds @ sl) 286 Density Impulse (kg · s · l @ sl) 342 Effective Velocity (exhaust m / s) 2,803 Reference Velocity (exhaust m / s) 1,771 Chamber Temperature (K) 3,137 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.19 |
NTO-Hydrogen
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2,015’88
Mixture Ratio (X:1)
6.50
Specific Impulse (seconds @ sl)
340
Density Impulse (kg · s · l @ sl)
137
Effective Velocity (exhaust m / s)
3,334
Reference Velocity (exhaust m / s)
2,103
Chamber Temperature (K)
2,973
Exhaust Weight (g / mole)
13.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.40
| NTO-Hydrogen ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2,015’88 Mixture Ratio (X:1) 6.50 Specific Impulse (seconds @ sl) 340 Density Impulse (kg · s · l @ sl) 137 Effective Velocity (exhaust m / s) 3,334 Reference Velocity (exhaust m / s) 2,103 Chamber Temperature (K) 2,973 Exhaust Weight (g / mole) 13.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.40 |
NTO-Hydrogen
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2,015’88
Mixture Ratio (X:1)
6.50
Specific Impulse (seconds @ sl)
340
Density Impulse (kg · s · l @ sl)
137
Effective Velocity (exhaust m / s)
3,334
Reference Velocity (exhaust m / s)
2,103
Chamber Temperature (K)
2,973
Exhaust Weight (g / mole)
13.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.40
| NTO-Hydrogen ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2,015’88 Mixture Ratio (X:1) 6.50 Specific Impulse (seconds @ sl) 340 Density Impulse (kg · s · l @ sl) 137 Effective Velocity (exhaust m / s) 3,334 Reference Velocity (exhaust m / s) 2,103 Chamber Temperature (K) 2,973 Exhaust Weight (g / mole) 13.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.40 |
NTO-Hydrogen
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2,015’88
Mixture Ratio (X:1)
6.50
Specific Impulse (seconds @ sl)
340
Density Impulse (kg · s · l @ sl)
137
Effective Velocity (exhaust m / s)
3,334
Reference Velocity (exhaust m / s)
2,103
Chamber Temperature (K)
2,973
Exhaust Weight (g / mole)
13.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.40
| NTO-Hydrogen ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2,015’88 Mixture Ratio (X:1) 6.50 Specific Impulse (seconds @ sl) 340 Density Impulse (kg · s · l @ sl) 137 Effective Velocity (exhaust m / s) 3,334 Reference Velocity (exhaust m / s) 2,103 Chamber Temperature (K) 2,973 Exhaust Weight (g / mole) 13.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.40 |
NTO-Hydrogen
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2,015’88
Mixture Ratio (X:1)
6.50
Specific Impulse (seconds @ sl)
340
Density Impulse (kg · s · l @ sl)
137
Effective Velocity (exhaust m / s)
3,334
Reference Velocity (exhaust m / s)
2,103
Chamber Temperature (K)
2,973
Exhaust Weight (g / mole)
13.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.40
| NTO-Hydrogen ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2,015’88 Mixture Ratio (X:1) 6.50 Specific Impulse (seconds @ sl) 340 Density Impulse (kg · s · l @ sl) 137 Effective Velocity (exhaust m / s) 3,334 Reference Velocity (exhaust m / s) 2,103 Chamber Temperature (K) 2,973 Exhaust Weight (g / mole) 13.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.40 |
NTO-Hydrogen
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2,015’88
Mixture Ratio (X:1)
6.50
Specific Impulse (seconds @ sl)
340
Density Impulse (kg · s · l @ sl)
137
Effective Velocity (exhaust m / s)
3,334
Reference Velocity (exhaust m / s)
2,103
Chamber Temperature (K)
2,973
Exhaust Weight (g / mole)
13.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.40
| NTO-Hydrogen ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2,015’88 Mixture Ratio (X:1) 6.50 Specific Impulse (seconds @ sl) 340 Density Impulse (kg · s · l @ sl) 137 Effective Velocity (exhaust m / s) 3,334 Reference Velocity (exhaust m / s) 2,103 Chamber Temperature (K) 2,973 Exhaust Weight (g / mole) 13.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.40 |
NTO-Kerosene
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.53
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
330
Effective Velocity (exhaust m / s)
2,619
Reference Velocity (exhaust m / s)
1,653
Chamber Temperature (K)
3,342
Exhaust Weight (g / mole)
23.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| NTO-Kerosene ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1 Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.53 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 330 Effective Velocity (exhaust m / s) 2,619 Reference Velocity (exhaust m / s) 1,653 Chamber Temperature (K) 3,342 Exhaust Weight (g / mole) 23.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
NTO-Kerosene
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.53
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
330
Effective Velocity (exhaust m / s)
2,619
Reference Velocity (exhaust m / s)
1,653
Chamber Temperature (K)
3,342
Exhaust Weight (g / mole)
23.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| NTO-Kerosene ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1 Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.53 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 330 Effective Velocity (exhaust m / s) 2,619 Reference Velocity (exhaust m / s) 1,653 Chamber Temperature (K) 3,342 Exhaust Weight (g / mole) 23.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
NTO-Kerosene
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.53
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
330
Effective Velocity (exhaust m / s)
2,619
Reference Velocity (exhaust m / s)
1,653
Chamber Temperature (K)
3,342
Exhaust Weight (g / mole)
23.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| NTO-Kerosene ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1 Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.53 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 330 Effective Velocity (exhaust m / s) 2,619 Reference Velocity (exhaust m / s) 1,653 Chamber Temperature (K) 3,342 Exhaust Weight (g / mole) 23.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
NTO-Kerosene
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.53
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
330
Effective Velocity (exhaust m / s)
2,619
Reference Velocity (exhaust m / s)
1,653
Chamber Temperature (K)
3,342
Exhaust Weight (g / mole)
23.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| NTO-Kerosene ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1 Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.53 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 330 Effective Velocity (exhaust m / s) 2,619 Reference Velocity (exhaust m / s) 1,653 Chamber Temperature (K) 3,342 Exhaust Weight (g / mole) 23.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
NTO-Kerosene
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.53
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
330
Effective Velocity (exhaust m / s)
2,619
Reference Velocity (exhaust m / s)
1,653
Chamber Temperature (K)
3,342
Exhaust Weight (g / mole)
23.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| NTO-Kerosene ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ RP-1 Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.53 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 330 Effective Velocity (exhaust m / s) 2,619 Reference Velocity (exhaust m / s) 1,653 Chamber Temperature (K) 3,342 Exhaust Weight (g / mole) 23.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
NTO-Methane
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
4.27
Specific Impulse (seconds @ sl)
273
Density Impulse (kg · s · l @ sl)
271
Effective Velocity (exhaust m / s)
2,682
Reference Velocity (exhaust m / s)
1,688
Chamber Temperature (K)
3,220
Exhaust Weight (g / mole)
22.10
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.99
| NTO-Methane ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 4.27 Specific Impulse (seconds @ sl) 273 Density Impulse (kg · s · l @ sl) 271 Effective Velocity (exhaust m / s) 2,682 Reference Velocity (exhaust m / s) 1,688 Chamber Temperature (K) 3,220 Exhaust Weight (g / mole) 22.10 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.99 |
NTO-Methane
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
4.27
Specific Impulse (seconds @ sl)
273
Density Impulse (kg · s · l @ sl)
271
Effective Velocity (exhaust m / s)
2,682
Reference Velocity (exhaust m / s)
1,688
Chamber Temperature (K)
3,220
Exhaust Weight (g / mole)
22.10
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.99
| NTO-Methane ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 4.27 Specific Impulse (seconds @ sl) 273 Density Impulse (kg · s · l @ sl) 271 Effective Velocity (exhaust m / s) 2,682 Reference Velocity (exhaust m / s) 1,688 Chamber Temperature (K) 3,220 Exhaust Weight (g / mole) 22.10 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.99 |
NTO-Methane
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
4.27
Specific Impulse (seconds @ sl)
273
Density Impulse (kg · s · l @ sl)
271
Effective Velocity (exhaust m / s)
2,682
Reference Velocity (exhaust m / s)
1,688
Chamber Temperature (K)
3,220
Exhaust Weight (g / mole)
22.10
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.99
| NTO-Methane ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 4.27 Specific Impulse (seconds @ sl) 273 Density Impulse (kg · s · l @ sl) 271 Effective Velocity (exhaust m / s) 2,682 Reference Velocity (exhaust m / s) 1,688 Chamber Temperature (K) 3,220 Exhaust Weight (g / mole) 22.10 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.99 |
NTO-Methane
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
4.27
Specific Impulse (seconds @ sl)
273
Density Impulse (kg · s · l @ sl)
271
Effective Velocity (exhaust m / s)
2,682
Reference Velocity (exhaust m / s)
1,688
Chamber Temperature (K)
3,220
Exhaust Weight (g / mole)
22.10
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.99
| NTO-Methane ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 4.27 Specific Impulse (seconds @ sl) 273 Density Impulse (kg · s · l @ sl) 271 Effective Velocity (exhaust m / s) 2,682 Reference Velocity (exhaust m / s) 1,688 Chamber Temperature (K) 3,220 Exhaust Weight (g / mole) 22.10 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.99 |
NTO-Methane
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
4.27
Specific Impulse (seconds @ sl)
273
Density Impulse (kg · s · l @ sl)
271
Effective Velocity (exhaust m / s)
2,682
Reference Velocity (exhaust m / s)
1,688
Chamber Temperature (K)
3,220
Exhaust Weight (g / mole)
22.10
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.99
| NTO-Methane ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 4.27 Specific Impulse (seconds @ sl) 273 Density Impulse (kg · s · l @ sl) 271 Effective Velocity (exhaust m / s) 2,682 Reference Velocity (exhaust m / s) 1,688 Chamber Temperature (K) 3,220 Exhaust Weight (g / mole) 22.10 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.99 |
NTO-Methanol
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.78
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,583
Chamber Temperature (K)
3,058
Exhaust Weight (g / mole)
24.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.12
| NTO-Methanol ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.78 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,583 Chamber Temperature (K) 3,058 Exhaust Weight (g / mole) 24.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.12 |
NTO-Methanol
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.78
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,583
Chamber Temperature (K)
3,058
Exhaust Weight (g / mole)
24.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.12
| NTO-Methanol ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.78 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,583 Chamber Temperature (K) 3,058 Exhaust Weight (g / mole) 24.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.12 |
NTO-Methanol
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.78
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,583
Chamber Temperature (K)
3,058
Exhaust Weight (g / mole)
24.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.12
| NTO-Methanol ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.78 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,583 Chamber Temperature (K) 3,058 Exhaust Weight (g / mole) 24.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.12 |
NTO-Methanol
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.78
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,583
Chamber Temperature (K)
3,058
Exhaust Weight (g / mole)
24.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.12
| NTO-Methanol ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.78 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,583 Chamber Temperature (K) 3,058 Exhaust Weight (g / mole) 24.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.12 |
NTO-Methanol
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.78
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,583
Chamber Temperature (K)
3,058
Exhaust Weight (g / mole)
24.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.12
| NTO-Methanol ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.78 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,583 Chamber Temperature (K) 3,058 Exhaust Weight (g / mole) 24.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.12 |
NTO-MMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.73
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
325
Effective Velocity (exhaust m / s)
2,742
Reference Velocity (exhaust m / s)
1,733
Chamber Temperature (K)
3,252
Exhaust Weight (g / mole)
21.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-MMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.73 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 325 Effective Velocity (exhaust m / s) 2,742 Reference Velocity (exhaust m / s) 1,733 Chamber Temperature (K) 3,252 Exhaust Weight (g / mole) 21.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-MMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.73
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
325
Effective Velocity (exhaust m / s)
2,742
Reference Velocity (exhaust m / s)
1,733
Chamber Temperature (K)
3,252
Exhaust Weight (g / mole)
21.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-MMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.73 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 325 Effective Velocity (exhaust m / s) 2,742 Reference Velocity (exhaust m / s) 1,733 Chamber Temperature (K) 3,252 Exhaust Weight (g / mole) 21.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-MMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.73
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
325
Effective Velocity (exhaust m / s)
2,742
Reference Velocity (exhaust m / s)
1,733
Chamber Temperature (K)
3,252
Exhaust Weight (g / mole)
21.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-MMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.73 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 325 Effective Velocity (exhaust m / s) 2,742 Reference Velocity (exhaust m / s) 1,733 Chamber Temperature (K) 3,252 Exhaust Weight (g / mole) 21.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-MMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.73
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
325
Effective Velocity (exhaust m / s)
2,742
Reference Velocity (exhaust m / s)
1,733
Chamber Temperature (K)
3,252
Exhaust Weight (g / mole)
21.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-MMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.73 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 325 Effective Velocity (exhaust m / s) 2,742 Reference Velocity (exhaust m / s) 1,733 Chamber Temperature (K) 3,252 Exhaust Weight (g / mole) 21.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-MMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.73
Specific Impulse (seconds @ sl)
280
Density Impulse (kg · s · l @ sl)
325
Effective Velocity (exhaust m / s)
2,742
Reference Velocity (exhaust m / s)
1,733
Chamber Temperature (K)
3,252
Exhaust Weight (g / mole)
21.10
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.16
| NTO-MMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.73 Specific Impulse (seconds @ sl) 280 Density Impulse (kg · s · l @ sl) 325 Effective Velocity (exhaust m / s) 2,742 Reference Velocity (exhaust m / s) 1,733 Chamber Temperature (K) 3,252 Exhaust Weight (g / mole) 21.10 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.16 |
NTO-Tonka-250
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.03
Specific Impulse (seconds @ sl)
264
Density Impulse (kg · s · l @ sl)
323
Effective Velocity (exhaust m / s)
2,585
Reference Velocity (exhaust m / s)
1,633
Chamber Temperature (K)
3,360
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.23
| NTO-Tonka-250 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.03 Specific Impulse (seconds @ sl) 264 Density Impulse (kg · s · l @ sl) 323 Effective Velocity (exhaust m / s) 2,585 Reference Velocity (exhaust m / s) 1,633 Chamber Temperature (K) 3,360 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.23 |
NTO-Tonka-250
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.03
Specific Impulse (seconds @ sl)
264
Density Impulse (kg · s · l @ sl)
323
Effective Velocity (exhaust m / s)
2,585
Reference Velocity (exhaust m / s)
1,633
Chamber Temperature (K)
3,360
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.23
| NTO-Tonka-250 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.03 Specific Impulse (seconds @ sl) 264 Density Impulse (kg · s · l @ sl) 323 Effective Velocity (exhaust m / s) 2,585 Reference Velocity (exhaust m / s) 1,633 Chamber Temperature (K) 3,360 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.23 |
NTO-Tonka-250
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.03
Specific Impulse (seconds @ sl)
264
Density Impulse (kg · s · l @ sl)
323
Effective Velocity (exhaust m / s)
2,585
Reference Velocity (exhaust m / s)
1,633
Chamber Temperature (K)
3,360
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.23
| NTO-Tonka-250 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.03 Specific Impulse (seconds @ sl) 264 Density Impulse (kg · s · l @ sl) 323 Effective Velocity (exhaust m / s) 2,585 Reference Velocity (exhaust m / s) 1,633 Chamber Temperature (K) 3,360 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.23 |
NTO-Tonka-250
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.03
Specific Impulse (seconds @ sl)
264
Density Impulse (kg · s · l @ sl)
323
Effective Velocity (exhaust m / s)
2,585
Reference Velocity (exhaust m / s)
1,633
Chamber Temperature (K)
3,360
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.23
| NTO-Tonka-250 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.03 Specific Impulse (seconds @ sl) 264 Density Impulse (kg · s · l @ sl) 323 Effective Velocity (exhaust m / s) 2,585 Reference Velocity (exhaust m / s) 1,633 Chamber Temperature (K) 3,360 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.23 |
NTO-Tonka-250
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.03
Specific Impulse (seconds @ sl)
264
Density Impulse (kg · s · l @ sl)
323
Effective Velocity (exhaust m / s)
2,585
Reference Velocity (exhaust m / s)
1,633
Chamber Temperature (K)
3,360
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.23
| NTO-Tonka-250 ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.03 Specific Impulse (seconds @ sl) 264 Density Impulse (kg · s · l @ sl) 323 Effective Velocity (exhaust m / s) 2,585 Reference Velocity (exhaust m / s) 1,633 Chamber Temperature (K) 3,360 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.23 |
NTO-UDMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.10
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
316
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,715
Chamber Temperature (K)
3,296
Exhaust Weight (g / mole)
21.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.14
| NTO-UDMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.10 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 316 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,715 Chamber Temperature (K) 3,296 Exhaust Weight (g / mole) 21.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.14 |
NTO-UDMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.10
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
316
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,715
Chamber Temperature (K)
3,296
Exhaust Weight (g / mole)
21.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.14
| NTO-UDMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.10 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 316 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,715 Chamber Temperature (K) 3,296 Exhaust Weight (g / mole) 21.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.14 |
NTO-UDMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.10
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
316
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,715
Chamber Temperature (K)
3,296
Exhaust Weight (g / mole)
21.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.14
| NTO-UDMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.10 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 316 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,715 Chamber Temperature (K) 3,296 Exhaust Weight (g / mole) 21.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.14 |
NTO-UDMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.10
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
316
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,715
Chamber Temperature (K)
3,296
Exhaust Weight (g / mole)
21.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.14
| NTO-UDMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.10 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 316 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,715 Chamber Temperature (K) 3,296 Exhaust Weight (g / mole) 21.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.14 |
NTO-UDMH
${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrogen Tetroxide
${ N }_{ 2 }{ O }_{ 4 }$
Molecular Weight (Oxidiser)
92.011’00
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.10
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
316
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,715
Chamber Temperature (K)
3,296
Exhaust Weight (g / mole)
21.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.14
| NTO-UDMH ${ N }_{ 2 }{ O }_{ 4 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrogen Tetroxide ${ N }_{ 2 }{ O }_{ 4 }$ Molecular Weight (Oxidiser) 92.011’00 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.10 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 316 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,715 Chamber Temperature (K) 3,296 Exhaust Weight (g / mole) 21.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.14 |