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
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOX, Oxygen
LOx-Aerozine-25
${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.22
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,928
Reference Velocity (exhaust m / s)
1,848
Chamber Temperature (K)
3,412
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.98
| LOx-Aerozine-25 ${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.22 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,928 Reference Velocity (exhaust m / s) 1,848 Chamber Temperature (K) 3,412 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.98 |
LOx-Aerozine-25
${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.22
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,928
Reference Velocity (exhaust m / s)
1,848
Chamber Temperature (K)
3,412
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.98
| LOx-Aerozine-25 ${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.22 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,928 Reference Velocity (exhaust m / s) 1,848 Chamber Temperature (K) 3,412 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.98 |
LOx-Aerozine-25
${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.22
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,928
Reference Velocity (exhaust m / s)
1,848
Chamber Temperature (K)
3,412
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.98
| LOx-Aerozine-25 ${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.22 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,928 Reference Velocity (exhaust m / s) 1,848 Chamber Temperature (K) 3,412 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.98 |
LOx-Aerozine-25
${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.22
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,928
Reference Velocity (exhaust m / s)
1,848
Chamber Temperature (K)
3,412
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.98
| LOx-Aerozine-25 ${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.22 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,928 Reference Velocity (exhaust m / s) 1,848 Chamber Temperature (K) 3,412 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.98 |
LOx-Aerozine-25
${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.22
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,928
Reference Velocity (exhaust m / s)
1,848
Chamber Temperature (K)
3,412
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.98
| LOx-Aerozine-25 ${ O }_{ 2 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.22 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,928 Reference Velocity (exhaust m / s) 1,848 Chamber Temperature (K) 3,412 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.98 |
LOx-Aerozine-50
${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.06
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,941
Reference Velocity (exhaust m / s)
1,856
Chamber Temperature (K)
3,373
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.00
| LOx-Aerozine-50 ${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.06 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,941 Reference Velocity (exhaust m / s) 1,856 Chamber Temperature (K) 3,373 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.00 |
LOx-Aerozine-50
${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.06
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,941
Reference Velocity (exhaust m / s)
1,856
Chamber Temperature (K)
3,373
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.00
| LOx-Aerozine-50 ${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.06 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,941 Reference Velocity (exhaust m / s) 1,856 Chamber Temperature (K) 3,373 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.00 |
LOx-Aerozine-50
${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.06
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,941
Reference Velocity (exhaust m / s)
1,856
Chamber Temperature (K)
3,373
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.00
| LOx-Aerozine-50 ${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.06 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,941 Reference Velocity (exhaust m / s) 1,856 Chamber Temperature (K) 3,373 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.00 |
LOx-Aerozine-50
${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.06
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,941
Reference Velocity (exhaust m / s)
1,856
Chamber Temperature (K)
3,373
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.00
| LOx-Aerozine-50 ${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.06 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,941 Reference Velocity (exhaust m / s) 1,856 Chamber Temperature (K) 3,373 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.00 |
LOx-Aerozine-50
${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.06
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
300
Effective Velocity (exhaust m / s)
2,941
Reference Velocity (exhaust m / s)
1,856
Chamber Temperature (K)
3,373
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.00
| LOx-Aerozine-50 ${ O }_{ 2 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.06 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 300 Effective Velocity (exhaust m / s) 2,941 Reference Velocity (exhaust m / s) 1,856 Chamber Temperature (K) 3,373 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.00 |
LOx-Ammonia
${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
287
Density Impulse (kg · s · l @ sl)
253
Effective Velocity (exhaust m / s)
2,815
Reference Velocity (exhaust m / s)
1,765
Chamber Temperature (K)
3,020
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.88
| LOx-Ammonia ${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 287 Density Impulse (kg · s · l @ sl) 253 Effective Velocity (exhaust m / s) 2,815 Reference Velocity (exhaust m / s) 1,765 Chamber Temperature (K) 3,020 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.88 |
LOx-Ammonia
${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
287
Density Impulse (kg · s · l @ sl)
253
Effective Velocity (exhaust m / s)
2,815
Reference Velocity (exhaust m / s)
1,765
Chamber Temperature (K)
3,020
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.88
| LOx-Ammonia ${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 287 Density Impulse (kg · s · l @ sl) 253 Effective Velocity (exhaust m / s) 2,815 Reference Velocity (exhaust m / s) 1,765 Chamber Temperature (K) 3,020 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.88 |
LOx-Ammonia
${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
287
Density Impulse (kg · s · l @ sl)
253
Effective Velocity (exhaust m / s)
2,815
Reference Velocity (exhaust m / s)
1,765
Chamber Temperature (K)
3,020
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.88
| LOx-Ammonia ${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 287 Density Impulse (kg · s · l @ sl) 253 Effective Velocity (exhaust m / s) 2,815 Reference Velocity (exhaust m / s) 1,765 Chamber Temperature (K) 3,020 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.88 |
LOx-Ammonia
${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
287
Density Impulse (kg · s · l @ sl)
253
Effective Velocity (exhaust m / s)
2,815
Reference Velocity (exhaust m / s)
1,765
Chamber Temperature (K)
3,020
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.88
| LOx-Ammonia ${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 287 Density Impulse (kg · s · l @ sl) 253 Effective Velocity (exhaust m / s) 2,815 Reference Velocity (exhaust m / s) 1,765 Chamber Temperature (K) 3,020 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.88 |
LOx-Ammonia
${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
287
Density Impulse (kg · s · l @ sl)
253
Effective Velocity (exhaust m / s)
2,815
Reference Velocity (exhaust m / s)
1,765
Chamber Temperature (K)
3,020
Exhaust Weight (g / mole)
19.10
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.88
| LOx-Ammonia ${ O }_{ 2 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 287 Density Impulse (kg · s · l @ sl) 253 Effective Velocity (exhaust m / s) 2,815 Reference Velocity (exhaust m / s) 1,765 Chamber Temperature (K) 3,020 Exhaust Weight (g / mole) 19.10 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.88 |
LOx-Aniline
${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
1.72
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
302
Effective Velocity (exhaust m / s)
2,708
Reference Velocity (exhaust m / s)
1,714
Chamber Temperature (K)
3,657
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.09
| LOx-Aniline ${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 1.72 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 302 Effective Velocity (exhaust m / s) 2,708 Reference Velocity (exhaust m / s) 1,714 Chamber Temperature (K) 3,657 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.09 |
LOx-Aniline
${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
1.72
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
302
Effective Velocity (exhaust m / s)
2,708
Reference Velocity (exhaust m / s)
1,714
Chamber Temperature (K)
3,657
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.09
| LOx-Aniline ${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 1.72 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 302 Effective Velocity (exhaust m / s) 2,708 Reference Velocity (exhaust m / s) 1,714 Chamber Temperature (K) 3,657 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.09 |
LOx-Aniline
${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
1.72
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
302
Effective Velocity (exhaust m / s)
2,708
Reference Velocity (exhaust m / s)
1,714
Chamber Temperature (K)
3,657
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.09
| LOx-Aniline ${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 1.72 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 302 Effective Velocity (exhaust m / s) 2,708 Reference Velocity (exhaust m / s) 1,714 Chamber Temperature (K) 3,657 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.09 |
LOx-Aniline
${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
1.72
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
302
Effective Velocity (exhaust m / s)
2,708
Reference Velocity (exhaust m / s)
1,714
Chamber Temperature (K)
3,657
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.09
| LOx-Aniline ${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 1.72 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 302 Effective Velocity (exhaust m / s) 2,708 Reference Velocity (exhaust m / s) 1,714 Chamber Temperature (K) 3,657 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.09 |
LOx-Aniline
${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
1.72
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
302
Effective Velocity (exhaust m / s)
2,708
Reference Velocity (exhaust m / s)
1,714
Chamber Temperature (K)
3,657
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.09
| LOx-Aniline ${ O }_{ 2 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 1.72 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 302 Effective Velocity (exhaust m / s) 2,708 Reference Velocity (exhaust m / s) 1,714 Chamber Temperature (K) 3,657 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.09 |
LOx-Ethanol-75
${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.29
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
264
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,643
Chamber Temperature (K)
3,167
Exhaust Weight (g / mole)
23.40
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.98
| LOx-Ethanol-75 ${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.29 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 264 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,643 Chamber Temperature (K) 3,167 Exhaust Weight (g / mole) 23.40 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.98 |
LOx-Ethanol-75
${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.29
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
264
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,643
Chamber Temperature (K)
3,167
Exhaust Weight (g / mole)
23.40
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.98
| LOx-Ethanol-75 ${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.29 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 264 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,643 Chamber Temperature (K) 3,167 Exhaust Weight (g / mole) 23.40 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.98 |
LOx-Ethanol-75
${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.29
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
264
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,643
Chamber Temperature (K)
3,167
Exhaust Weight (g / mole)
23.40
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.98
| LOx-Ethanol-75 ${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.29 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 264 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,643 Chamber Temperature (K) 3,167 Exhaust Weight (g / mole) 23.40 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.98 |
LOx-Ethanol-75
${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.29
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
264
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,643
Chamber Temperature (K)
3,167
Exhaust Weight (g / mole)
23.40
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.98
| LOx-Ethanol-75 ${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.29 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 264 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,643 Chamber Temperature (K) 3,167 Exhaust Weight (g / mole) 23.40 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.98 |
LOx-Ethanol-75
${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.29
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
264
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,643
Chamber Temperature (K)
3,167
Exhaust Weight (g / mole)
23.40
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.98
| LOx-Ethanol-75 ${ O }_{ 2 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.29 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 264 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,643 Chamber Temperature (K) 3,167 Exhaust Weight (g / mole) 23.40 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.98 |
LOx-Ethanol-95
${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.49
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
269
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,698
Chamber Temperature (K)
3,314
Exhaust Weight (g / mole)
22.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.97
| LOx-Ethanol-95 ${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.49 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 269 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,698 Chamber Temperature (K) 3,314 Exhaust Weight (g / mole) 22.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.97 |
LOx-Ethanol-95
${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.49
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
269
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,698
Chamber Temperature (K)
3,314
Exhaust Weight (g / mole)
22.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.97
| LOx-Ethanol-95 ${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.49 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 269 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,698 Chamber Temperature (K) 3,314 Exhaust Weight (g / mole) 22.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.97 |
LOx-Ethanol-95
${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.49
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
269
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,698
Chamber Temperature (K)
3,314
Exhaust Weight (g / mole)
22.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.97
| LOx-Ethanol-95 ${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.49 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 269 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,698 Chamber Temperature (K) 3,314 Exhaust Weight (g / mole) 22.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.97 |
LOx-Ethanol-95
${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.49
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
269
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,698
Chamber Temperature (K)
3,314
Exhaust Weight (g / mole)
22.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.97
| LOx-Ethanol-95 ${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.49 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 269 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,698 Chamber Temperature (K) 3,314 Exhaust Weight (g / mole) 22.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.97 |
LOx-Ethanol-95
${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.49
Specific Impulse (seconds @ sl)
277
Density Impulse (kg · s · l @ sl)
269
Effective Velocity (exhaust m / s)
2,713
Reference Velocity (exhaust m / s)
1,698
Chamber Temperature (K)
3,314
Exhaust Weight (g / mole)
22.80
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
0.97
| LOx-Ethanol-95 ${ O }_{ 2 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.49 Specific Impulse (seconds @ sl) 277 Density Impulse (kg · s · l @ sl) 269 Effective Velocity (exhaust m / s) 2,713 Reference Velocity (exhaust m / s) 1,698 Chamber Temperature (K) 3,314 Exhaust Weight (g / mole) 22.80 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 0.97 |
LOx-HTPB
${ O }_{ 2 }$ ⋅ HTPB
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
2.12
Specific Impulse (seconds @ sl)
282
Density Impulse (kg · s · l @ sl)
299
Effective Velocity (exhaust m / s)
2,766
Reference Velocity (exhaust m / s)
1,747
Chamber Temperature (K)
3,612
Exhaust Weight (g / mole)
23.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-HTPB ${ O }_{ 2 }$ ⋅ HTPB Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 2.12 Specific Impulse (seconds @ sl) 282 Density Impulse (kg · s · l @ sl) 299 Effective Velocity (exhaust m / s) 2,766 Reference Velocity (exhaust m / s) 1,747 Chamber Temperature (K) 3,612 Exhaust Weight (g / mole) 23.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-HTPB
${ O }_{ 2 }$ ⋅ HTPB
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
2.12
Specific Impulse (seconds @ sl)
282
Density Impulse (kg · s · l @ sl)
299
Effective Velocity (exhaust m / s)
2,766
Reference Velocity (exhaust m / s)
1,747
Chamber Temperature (K)
3,612
Exhaust Weight (g / mole)
23.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-HTPB ${ O }_{ 2 }$ ⋅ HTPB Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 2.12 Specific Impulse (seconds @ sl) 282 Density Impulse (kg · s · l @ sl) 299 Effective Velocity (exhaust m / s) 2,766 Reference Velocity (exhaust m / s) 1,747 Chamber Temperature (K) 3,612 Exhaust Weight (g / mole) 23.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-HTPB
${ O }_{ 2 }$ ⋅ HTPB
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
2.12
Specific Impulse (seconds @ sl)
282
Density Impulse (kg · s · l @ sl)
299
Effective Velocity (exhaust m / s)
2,766
Reference Velocity (exhaust m / s)
1,747
Chamber Temperature (K)
3,612
Exhaust Weight (g / mole)
23.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-HTPB ${ O }_{ 2 }$ ⋅ HTPB Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 2.12 Specific Impulse (seconds @ sl) 282 Density Impulse (kg · s · l @ sl) 299 Effective Velocity (exhaust m / s) 2,766 Reference Velocity (exhaust m / s) 1,747 Chamber Temperature (K) 3,612 Exhaust Weight (g / mole) 23.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-HTPB
${ O }_{ 2 }$ ⋅ HTPB
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
2.12
Specific Impulse (seconds @ sl)
282
Density Impulse (kg · s · l @ sl)
299
Effective Velocity (exhaust m / s)
2,766
Reference Velocity (exhaust m / s)
1,747
Chamber Temperature (K)
3,612
Exhaust Weight (g / mole)
23.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-HTPB ${ O }_{ 2 }$ ⋅ HTPB Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 2.12 Specific Impulse (seconds @ sl) 282 Density Impulse (kg · s · l @ sl) 299 Effective Velocity (exhaust m / s) 2,766 Reference Velocity (exhaust m / s) 1,747 Chamber Temperature (K) 3,612 Exhaust Weight (g / mole) 23.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-HTPB
${ O }_{ 2 }$ ⋅ HTPB
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
2.12
Specific Impulse (seconds @ sl)
282
Density Impulse (kg · s · l @ sl)
299
Effective Velocity (exhaust m / s)
2,766
Reference Velocity (exhaust m / s)
1,747
Chamber Temperature (K)
3,612
Exhaust Weight (g / mole)
23.10
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-HTPB ${ O }_{ 2 }$ ⋅ HTPB Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 2.12 Specific Impulse (seconds @ sl) 282 Density Impulse (kg · s · l @ sl) 299 Effective Velocity (exhaust m / s) 2,766 Reference Velocity (exhaust m / s) 1,747 Chamber Temperature (K) 3,612 Exhaust Weight (g / mole) 23.10 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-Hydrazine
${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
0.74
Specific Impulse (seconds @ sl)
303
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,973
Reference Velocity (exhaust m / s)
1,875
Chamber Temperature (K)
3,275
Exhaust Weight (g / mole)
18.20
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-Hydrazine ${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 0.74 Specific Impulse (seconds @ sl) 303 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,973 Reference Velocity (exhaust m / s) 1,875 Chamber Temperature (K) 3,275 Exhaust Weight (g / mole) 18.20 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-Hydrazine
${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
0.74
Specific Impulse (seconds @ sl)
303
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,973
Reference Velocity (exhaust m / s)
1,875
Chamber Temperature (K)
3,275
Exhaust Weight (g / mole)
18.20
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-Hydrazine ${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 0.74 Specific Impulse (seconds @ sl) 303 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,973 Reference Velocity (exhaust m / s) 1,875 Chamber Temperature (K) 3,275 Exhaust Weight (g / mole) 18.20 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-Hydrazine
${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
0.74
Specific Impulse (seconds @ sl)
303
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,973
Reference Velocity (exhaust m / s)
1,875
Chamber Temperature (K)
3,275
Exhaust Weight (g / mole)
18.20
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-Hydrazine ${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 0.74 Specific Impulse (seconds @ sl) 303 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,973 Reference Velocity (exhaust m / s) 1,875 Chamber Temperature (K) 3,275 Exhaust Weight (g / mole) 18.20 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-Hydrazine
${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
0.74
Specific Impulse (seconds @ sl)
303
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,973
Reference Velocity (exhaust m / s)
1,875
Chamber Temperature (K)
3,275
Exhaust Weight (g / mole)
18.20
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-Hydrazine ${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 0.74 Specific Impulse (seconds @ sl) 303 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,973 Reference Velocity (exhaust m / s) 1,875 Chamber Temperature (K) 3,275 Exhaust Weight (g / mole) 18.20 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-Hydrazine
${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
0.74
Specific Impulse (seconds @ sl)
303
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,973
Reference Velocity (exhaust m / s)
1,875
Chamber Temperature (K)
3,275
Exhaust Weight (g / mole)
18.20
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.06
| LOx-Hydrazine ${ O }_{ 2 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 0.74 Specific Impulse (seconds @ sl) 303 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,973 Reference Velocity (exhaust m / s) 1,875 Chamber Temperature (K) 3,275 Exhaust Weight (g / mole) 18.20 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.06 |
LOx-Hydrogen
${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydrogen [Hydrolox]
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
5.00
Specific Impulse (seconds @ sl)
381
Density Impulse (kg · s · l @ sl)
124
Effective Velocity (exhaust m / s)
3,738
Reference Velocity (exhaust m / s)
2,347
Chamber Temperature (K)
3,304
Exhaust Weight (g / mole)
11.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.32
| LOx-Hydrogen ${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydrogen [Hydrolox] ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 5.00 Specific Impulse (seconds @ sl) 381 Density Impulse (kg · s · l @ sl) 124 Effective Velocity (exhaust m / s) 3,738 Reference Velocity (exhaust m / s) 2,347 Chamber Temperature (K) 3,304 Exhaust Weight (g / mole) 11.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.32 |
LOx-Hydrogen
${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydrogen [Hydrolox]
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
5.00
Specific Impulse (seconds @ sl)
381
Density Impulse (kg · s · l @ sl)
124
Effective Velocity (exhaust m / s)
3,738
Reference Velocity (exhaust m / s)
2,347
Chamber Temperature (K)
3,304
Exhaust Weight (g / mole)
11.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.32
| LOx-Hydrogen ${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydrogen [Hydrolox] ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 5.00 Specific Impulse (seconds @ sl) 381 Density Impulse (kg · s · l @ sl) 124 Effective Velocity (exhaust m / s) 3,738 Reference Velocity (exhaust m / s) 2,347 Chamber Temperature (K) 3,304 Exhaust Weight (g / mole) 11.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.32 |
LOx-Hydrogen
${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydrogen [Hydrolox]
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
5.00
Specific Impulse (seconds @ sl)
381
Density Impulse (kg · s · l @ sl)
124
Effective Velocity (exhaust m / s)
3,738
Reference Velocity (exhaust m / s)
2,347
Chamber Temperature (K)
3,304
Exhaust Weight (g / mole)
11.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.32
| LOx-Hydrogen ${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydrogen [Hydrolox] ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 5.00 Specific Impulse (seconds @ sl) 381 Density Impulse (kg · s · l @ sl) 124 Effective Velocity (exhaust m / s) 3,738 Reference Velocity (exhaust m / s) 2,347 Chamber Temperature (K) 3,304 Exhaust Weight (g / mole) 11.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.32 |
LOx-Hydrogen
${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydrogen [Hydrolox]
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
5.00
Specific Impulse (seconds @ sl)
381
Density Impulse (kg · s · l @ sl)
124
Effective Velocity (exhaust m / s)
3,738
Reference Velocity (exhaust m / s)
2,347
Chamber Temperature (K)
3,304
Exhaust Weight (g / mole)
11.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.32
| LOx-Hydrogen ${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydrogen [Hydrolox] ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 5.00 Specific Impulse (seconds @ sl) 381 Density Impulse (kg · s · l @ sl) 124 Effective Velocity (exhaust m / s) 3,738 Reference Velocity (exhaust m / s) 2,347 Chamber Temperature (K) 3,304 Exhaust Weight (g / mole) 11.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.32 |
LOx-Hydrogen
${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Hydrogen [Hydrolox]
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
5.00
Specific Impulse (seconds @ sl)
381
Density Impulse (kg · s · l @ sl)
124
Effective Velocity (exhaust m / s)
3,738
Reference Velocity (exhaust m / s)
2,347
Chamber Temperature (K)
3,304
Exhaust Weight (g / mole)
11.80
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.32
| LOx-Hydrogen ${ O }_{ 2 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Hydrogen [Hydrolox] ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 5.00 Specific Impulse (seconds @ sl) 381 Density Impulse (kg · s · l @ sl) 124 Effective Velocity (exhaust m / s) 3,738 Reference Velocity (exhaust m / s) 2,347 Chamber Temperature (K) 3,304 Exhaust Weight (g / mole) 11.80 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.32 |
LOx-Kerosene
${ O }_{ 2 }$ ⋅ RP-1
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Kerosene [Kerolox]
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
2.29
Specific Impulse (seconds @ sl)
289
Density Impulse (kg · s · l @ sl)
294
Effective Velocity (exhaust m / s)
2,834
Reference Velocity (exhaust m / s)
1,787
Chamber Temperature (K)
3,526
Exhaust Weight (g / mole)
21.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Kerosene ${ O }_{ 2 }$ ⋅ RP-1 Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Kerosene [Kerolox] RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 2.29 Specific Impulse (seconds @ sl) 289 Density Impulse (kg · s · l @ sl) 294 Effective Velocity (exhaust m / s) 2,834 Reference Velocity (exhaust m / s) 1,787 Chamber Temperature (K) 3,526 Exhaust Weight (g / mole) 21.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Kerosene
${ O }_{ 2 }$ ⋅ RP-1
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Kerosene [Kerolox]
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
2.29
Specific Impulse (seconds @ sl)
289
Density Impulse (kg · s · l @ sl)
294
Effective Velocity (exhaust m / s)
2,834
Reference Velocity (exhaust m / s)
1,787
Chamber Temperature (K)
3,526
Exhaust Weight (g / mole)
21.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Kerosene ${ O }_{ 2 }$ ⋅ RP-1 Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Kerosene [Kerolox] RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 2.29 Specific Impulse (seconds @ sl) 289 Density Impulse (kg · s · l @ sl) 294 Effective Velocity (exhaust m / s) 2,834 Reference Velocity (exhaust m / s) 1,787 Chamber Temperature (K) 3,526 Exhaust Weight (g / mole) 21.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Kerosene
${ O }_{ 2 }$ ⋅ RP-1
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Kerosene [Kerolox]
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
2.29
Specific Impulse (seconds @ sl)
289
Density Impulse (kg · s · l @ sl)
294
Effective Velocity (exhaust m / s)
2,834
Reference Velocity (exhaust m / s)
1,787
Chamber Temperature (K)
3,526
Exhaust Weight (g / mole)
21.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Kerosene ${ O }_{ 2 }$ ⋅ RP-1 Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Kerosene [Kerolox] RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 2.29 Specific Impulse (seconds @ sl) 289 Density Impulse (kg · s · l @ sl) 294 Effective Velocity (exhaust m / s) 2,834 Reference Velocity (exhaust m / s) 1,787 Chamber Temperature (K) 3,526 Exhaust Weight (g / mole) 21.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Kerosene
${ O }_{ 2 }$ ⋅ RP-1
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Kerosene [Kerolox]
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
2.29
Specific Impulse (seconds @ sl)
289
Density Impulse (kg · s · l @ sl)
294
Effective Velocity (exhaust m / s)
2,834
Reference Velocity (exhaust m / s)
1,787
Chamber Temperature (K)
3,526
Exhaust Weight (g / mole)
21.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Kerosene ${ O }_{ 2 }$ ⋅ RP-1 Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Kerosene [Kerolox] RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 2.29 Specific Impulse (seconds @ sl) 289 Density Impulse (kg · s · l @ sl) 294 Effective Velocity (exhaust m / s) 2,834 Reference Velocity (exhaust m / s) 1,787 Chamber Temperature (K) 3,526 Exhaust Weight (g / mole) 21.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Kerosene
${ O }_{ 2 }$ ⋅ RP-1
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Kerosene [Kerolox]
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
2.29
Specific Impulse (seconds @ sl)
289
Density Impulse (kg · s · l @ sl)
294
Effective Velocity (exhaust m / s)
2,834
Reference Velocity (exhaust m / s)
1,787
Chamber Temperature (K)
3,526
Exhaust Weight (g / mole)
21.60
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Kerosene ${ O }_{ 2 }$ ⋅ RP-1 Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Kerosene [Kerolox] RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 2.29 Specific Impulse (seconds @ sl) 289 Density Impulse (kg · s · l @ sl) 294 Effective Velocity (exhaust m / s) 2,834 Reference Velocity (exhaust m / s) 1,787 Chamber Temperature (K) 3,526 Exhaust Weight (g / mole) 21.60 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Methane
${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methane [Methalox]
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
2.77
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
235
Effective Velocity (exhaust m / s)
2,932
Reference Velocity (exhaust m / s)
1,842
Chamber Temperature (K)
3,379
Exhaust Weight (g / mole)
19.60
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.79
| LOx-Methane ${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methane [Methalox] ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 2.77 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 235 Effective Velocity (exhaust m / s) 2,932 Reference Velocity (exhaust m / s) 1,842 Chamber Temperature (K) 3,379 Exhaust Weight (g / mole) 19.60 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.79 |
LOx-Methane
${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methane [Methalox]
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
2.77
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
235
Effective Velocity (exhaust m / s)
2,932
Reference Velocity (exhaust m / s)
1,842
Chamber Temperature (K)
3,379
Exhaust Weight (g / mole)
19.60
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.79
| LOx-Methane ${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methane [Methalox] ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 2.77 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 235 Effective Velocity (exhaust m / s) 2,932 Reference Velocity (exhaust m / s) 1,842 Chamber Temperature (K) 3,379 Exhaust Weight (g / mole) 19.60 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.79 |
LOx-Methane
${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methane [Methalox]
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
2.77
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
235
Effective Velocity (exhaust m / s)
2,932
Reference Velocity (exhaust m / s)
1,842
Chamber Temperature (K)
3,379
Exhaust Weight (g / mole)
19.60
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.79
| LOx-Methane ${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methane [Methalox] ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 2.77 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 235 Effective Velocity (exhaust m / s) 2,932 Reference Velocity (exhaust m / s) 1,842 Chamber Temperature (K) 3,379 Exhaust Weight (g / mole) 19.60 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.79 |
LOx-Methane
${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methane [Methalox]
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
2.77
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
235
Effective Velocity (exhaust m / s)
2,932
Reference Velocity (exhaust m / s)
1,842
Chamber Temperature (K)
3,379
Exhaust Weight (g / mole)
19.60
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.79
| LOx-Methane ${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methane [Methalox] ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 2.77 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 235 Effective Velocity (exhaust m / s) 2,932 Reference Velocity (exhaust m / s) 1,842 Chamber Temperature (K) 3,379 Exhaust Weight (g / mole) 19.60 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.79 |
LOx-Methane
${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methane [Methalox]
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
2.77
Specific Impulse (seconds @ sl)
299
Density Impulse (kg · s · l @ sl)
235
Effective Velocity (exhaust m / s)
2,932
Reference Velocity (exhaust m / s)
1,842
Chamber Temperature (K)
3,379
Exhaust Weight (g / mole)
19.60
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.79
| LOx-Methane ${ O }_{ 2 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methane [Methalox] ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 2.77 Specific Impulse (seconds @ sl) 299 Density Impulse (kg · s · l @ sl) 235 Effective Velocity (exhaust m / s) 2,932 Reference Velocity (exhaust m / s) 1,842 Chamber Temperature (K) 3,379 Exhaust Weight (g / mole) 19.60 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.79 |
LOx-Methanol
${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.19
Specific Impulse (seconds @ sl)
274
Density Impulse (kg · s · l @ sl)
260
Effective Velocity (exhaust m / s)
2,687
Reference Velocity (exhaust m / s)
1,677
Chamber Temperature (K)
3,214
Exhaust Weight (g / mole)
22.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.95
| LOx-Methanol ${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.19 Specific Impulse (seconds @ sl) 274 Density Impulse (kg · s · l @ sl) 260 Effective Velocity (exhaust m / s) 2,687 Reference Velocity (exhaust m / s) 1,677 Chamber Temperature (K) 3,214 Exhaust Weight (g / mole) 22.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.95 |
LOx-Methanol
${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.19
Specific Impulse (seconds @ sl)
274
Density Impulse (kg · s · l @ sl)
260
Effective Velocity (exhaust m / s)
2,687
Reference Velocity (exhaust m / s)
1,677
Chamber Temperature (K)
3,214
Exhaust Weight (g / mole)
22.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.95
| LOx-Methanol ${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.19 Specific Impulse (seconds @ sl) 274 Density Impulse (kg · s · l @ sl) 260 Effective Velocity (exhaust m / s) 2,687 Reference Velocity (exhaust m / s) 1,677 Chamber Temperature (K) 3,214 Exhaust Weight (g / mole) 22.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.95 |
LOx-Methanol
${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.19
Specific Impulse (seconds @ sl)
274
Density Impulse (kg · s · l @ sl)
260
Effective Velocity (exhaust m / s)
2,687
Reference Velocity (exhaust m / s)
1,677
Chamber Temperature (K)
3,214
Exhaust Weight (g / mole)
22.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.95
| LOx-Methanol ${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.19 Specific Impulse (seconds @ sl) 274 Density Impulse (kg · s · l @ sl) 260 Effective Velocity (exhaust m / s) 2,687 Reference Velocity (exhaust m / s) 1,677 Chamber Temperature (K) 3,214 Exhaust Weight (g / mole) 22.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.95 |
LOx-Methanol
${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.19
Specific Impulse (seconds @ sl)
274
Density Impulse (kg · s · l @ sl)
260
Effective Velocity (exhaust m / s)
2,687
Reference Velocity (exhaust m / s)
1,677
Chamber Temperature (K)
3,214
Exhaust Weight (g / mole)
22.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.95
| LOx-Methanol ${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.19 Specific Impulse (seconds @ sl) 274 Density Impulse (kg · s · l @ sl) 260 Effective Velocity (exhaust m / s) 2,687 Reference Velocity (exhaust m / s) 1,677 Chamber Temperature (K) 3,214 Exhaust Weight (g / mole) 22.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.95 |
LOx-Methanol
${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
1.19
Specific Impulse (seconds @ sl)
274
Density Impulse (kg · s · l @ sl)
260
Effective Velocity (exhaust m / s)
2,687
Reference Velocity (exhaust m / s)
1,677
Chamber Temperature (K)
3,214
Exhaust Weight (g / mole)
22.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
0.95
| LOx-Methanol ${ O }_{ 2 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 1.19 Specific Impulse (seconds @ sl) 274 Density Impulse (kg · s · l @ sl) 260 Effective Velocity (exhaust m / s) 2,687 Reference Velocity (exhaust m / s) 1,677 Chamber Temperature (K) 3,214 Exhaust Weight (g / mole) 22.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 0.95 |
LOx-MMH
${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.15
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
298
Effective Velocity (exhaust m / s)
2,938
Reference Velocity (exhaust m / s)
1,855
Chamber Temperature (K)
3,399
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.99
| LOx-MMH ${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.15 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 298 Effective Velocity (exhaust m / s) 2,938 Reference Velocity (exhaust m / s) 1,855 Chamber Temperature (K) 3,399 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.99 |
LOx-MMH
${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.15
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
298
Effective Velocity (exhaust m / s)
2,938
Reference Velocity (exhaust m / s)
1,855
Chamber Temperature (K)
3,399
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.99
| LOx-MMH ${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.15 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 298 Effective Velocity (exhaust m / s) 2,938 Reference Velocity (exhaust m / s) 1,855 Chamber Temperature (K) 3,399 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.99 |
LOx-MMH
${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.15
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
298
Effective Velocity (exhaust m / s)
2,938
Reference Velocity (exhaust m / s)
1,855
Chamber Temperature (K)
3,399
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.99
| LOx-MMH ${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.15 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 298 Effective Velocity (exhaust m / s) 2,938 Reference Velocity (exhaust m / s) 1,855 Chamber Temperature (K) 3,399 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.99 |
LOx-MMH
${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.15
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
298
Effective Velocity (exhaust m / s)
2,938
Reference Velocity (exhaust m / s)
1,855
Chamber Temperature (K)
3,399
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.99
| LOx-MMH ${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.15 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 298 Effective Velocity (exhaust m / s) 2,938 Reference Velocity (exhaust m / s) 1,855 Chamber Temperature (K) 3,399 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.99 |
LOx-MMH
${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
1.15
Specific Impulse (seconds @ sl)
300
Density Impulse (kg · s · l @ sl)
298
Effective Velocity (exhaust m / s)
2,938
Reference Velocity (exhaust m / s)
1,855
Chamber Temperature (K)
3,399
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.99
| LOx-MMH ${ O }_{ 2 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 1.15 Specific Impulse (seconds @ sl) 300 Density Impulse (kg · s · l @ sl) 298 Effective Velocity (exhaust m / s) 2,938 Reference Velocity (exhaust m / s) 1,855 Chamber Temperature (K) 3,399 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.99 |
LOx-Tonka-250
${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.97
Specific Impulse (seconds @ sl)
283
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,780
Reference Velocity (exhaust m / s)
1,754
Chamber Temperature (K)
3,543
Exhaust Weight (g / mole)
22.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Tonka-250 ${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.97 Specific Impulse (seconds @ sl) 283 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,780 Reference Velocity (exhaust m / s) 1,754 Chamber Temperature (K) 3,543 Exhaust Weight (g / mole) 22.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Tonka-250
${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.97
Specific Impulse (seconds @ sl)
283
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,780
Reference Velocity (exhaust m / s)
1,754
Chamber Temperature (K)
3,543
Exhaust Weight (g / mole)
22.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Tonka-250 ${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.97 Specific Impulse (seconds @ sl) 283 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,780 Reference Velocity (exhaust m / s) 1,754 Chamber Temperature (K) 3,543 Exhaust Weight (g / mole) 22.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Tonka-250
${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.97
Specific Impulse (seconds @ sl)
283
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,780
Reference Velocity (exhaust m / s)
1,754
Chamber Temperature (K)
3,543
Exhaust Weight (g / mole)
22.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Tonka-250 ${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.97 Specific Impulse (seconds @ sl) 283 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,780 Reference Velocity (exhaust m / s) 1,754 Chamber Temperature (K) 3,543 Exhaust Weight (g / mole) 22.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Tonka-250
${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.97
Specific Impulse (seconds @ sl)
283
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,780
Reference Velocity (exhaust m / s)
1,754
Chamber Temperature (K)
3,543
Exhaust Weight (g / mole)
22.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Tonka-250 ${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.97 Specific Impulse (seconds @ sl) 283 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,780 Reference Velocity (exhaust m / s) 1,754 Chamber Temperature (K) 3,543 Exhaust Weight (g / mole) 22.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-Tonka-250
${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
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)
1.97
Specific Impulse (seconds @ sl)
283
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,780
Reference Velocity (exhaust m / s)
1,754
Chamber Temperature (K)
3,543
Exhaust Weight (g / mole)
22.50
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.02
| LOx-Tonka-250 ${ O }_{ 2 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 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) 1.97 Specific Impulse (seconds @ sl) 283 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,780 Reference Velocity (exhaust m / s) 1,754 Chamber Temperature (K) 3,543 Exhaust Weight (g / mole) 22.50 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.02 |
LOx-UDMH
${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
1.38
Specific Impulse (seconds @ sl)
297
Density Impulse (kg · s · l @ sl)
286
Effective Velocity (exhaust m / s)
2,916
Reference Velocity (exhaust m / s)
1,841
Chamber Temperature (K)
3,447
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.96
| LOx-UDMH ${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 1.38 Specific Impulse (seconds @ sl) 297 Density Impulse (kg · s · l @ sl) 286 Effective Velocity (exhaust m / s) 2,916 Reference Velocity (exhaust m / s) 1,841 Chamber Temperature (K) 3,447 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.96 |
LOx-UDMH
${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
1.38
Specific Impulse (seconds @ sl)
297
Density Impulse (kg · s · l @ sl)
286
Effective Velocity (exhaust m / s)
2,916
Reference Velocity (exhaust m / s)
1,841
Chamber Temperature (K)
3,447
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.96
| LOx-UDMH ${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 1.38 Specific Impulse (seconds @ sl) 297 Density Impulse (kg · s · l @ sl) 286 Effective Velocity (exhaust m / s) 2,916 Reference Velocity (exhaust m / s) 1,841 Chamber Temperature (K) 3,447 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.96 |
LOx-UDMH
${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
1.38
Specific Impulse (seconds @ sl)
297
Density Impulse (kg · s · l @ sl)
286
Effective Velocity (exhaust m / s)
2,916
Reference Velocity (exhaust m / s)
1,841
Chamber Temperature (K)
3,447
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.96
| LOx-UDMH ${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 1.38 Specific Impulse (seconds @ sl) 297 Density Impulse (kg · s · l @ sl) 286 Effective Velocity (exhaust m / s) 2,916 Reference Velocity (exhaust m / s) 1,841 Chamber Temperature (K) 3,447 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.96 |
LOx-UDMH
${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
1.38
Specific Impulse (seconds @ sl)
297
Density Impulse (kg · s · l @ sl)
286
Effective Velocity (exhaust m / s)
2,916
Reference Velocity (exhaust m / s)
1,841
Chamber Temperature (K)
3,447
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.96
| LOx-UDMH ${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 1.38 Specific Impulse (seconds @ sl) 297 Density Impulse (kg · s · l @ sl) 286 Effective Velocity (exhaust m / s) 2,916 Reference Velocity (exhaust m / s) 1,841 Chamber Temperature (K) 3,447 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.96 |
LOx-UDMH
${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Oxygen
${ O }_{ 2 }$
Molecular Weight (Oxidiser)
31.998’8
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
1.38
Specific Impulse (seconds @ sl)
297
Density Impulse (kg · s · l @ sl)
286
Effective Velocity (exhaust m / s)
2,916
Reference Velocity (exhaust m / s)
1,841
Chamber Temperature (K)
3,447
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
0.96
| LOx-UDMH ${ O }_{ 2 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Oxygen ${ O }_{ 2 }$ Molecular Weight (Oxidiser) 31.998’8 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 1.38 Specific Impulse (seconds @ sl) 297 Density Impulse (kg · s · l @ sl) 286 Effective Velocity (exhaust m / s) 2,916 Reference Velocity (exhaust m / s) 1,841 Chamber Temperature (K) 3,447 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 0.96 |