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
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO, Nitrous Oxide
NO-Aerozine-25
${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.57
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,543
Reference Velocity (exhaust m / s)
1,615
Chamber Temperature (K)
3,182
Exhaust Weight (g / mole)
23.50
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.11
| NO-Aerozine-25 ${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.57 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,543 Reference Velocity (exhaust m / s) 1,615 Chamber Temperature (K) 3,182 Exhaust Weight (g / mole) 23.50 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.11 |
NO-Aerozine-25
${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.57
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,543
Reference Velocity (exhaust m / s)
1,615
Chamber Temperature (K)
3,182
Exhaust Weight (g / mole)
23.50
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.11
| NO-Aerozine-25 ${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.57 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,543 Reference Velocity (exhaust m / s) 1,615 Chamber Temperature (K) 3,182 Exhaust Weight (g / mole) 23.50 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.11 |
NO-Aerozine-25
${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.57
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,543
Reference Velocity (exhaust m / s)
1,615
Chamber Temperature (K)
3,182
Exhaust Weight (g / mole)
23.50
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.11
| NO-Aerozine-25 ${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.57 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,543 Reference Velocity (exhaust m / s) 1,615 Chamber Temperature (K) 3,182 Exhaust Weight (g / mole) 23.50 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.11 |
NO-Aerozine-25
${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.57
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,543
Reference Velocity (exhaust m / s)
1,615
Chamber Temperature (K)
3,182
Exhaust Weight (g / mole)
23.50
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.11
| NO-Aerozine-25 ${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.57 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,543 Reference Velocity (exhaust m / s) 1,615 Chamber Temperature (K) 3,182 Exhaust Weight (g / mole) 23.50 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.11 |
NO-Aerozine-25
${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.57
Specific Impulse (seconds @ sl)
259
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,543
Reference Velocity (exhaust m / s)
1,615
Chamber Temperature (K)
3,182
Exhaust Weight (g / mole)
23.50
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.11
| NO-Aerozine-25 ${ N }_{ 2 }{ O }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.57 Specific Impulse (seconds @ sl) 259 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,543 Reference Velocity (exhaust m / s) 1,615 Chamber Temperature (K) 3,182 Exhaust Weight (g / mole) 23.50 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.11 |
NO-Aerozine-50
${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.04
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,563
Reference Velocity (exhaust m / s)
1,627
Chamber Temperature (K)
3,148
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-Aerozine-50 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.04 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,563 Reference Velocity (exhaust m / s) 1,627 Chamber Temperature (K) 3,148 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-Aerozine-50
${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.04
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,563
Reference Velocity (exhaust m / s)
1,627
Chamber Temperature (K)
3,148
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-Aerozine-50 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.04 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,563 Reference Velocity (exhaust m / s) 1,627 Chamber Temperature (K) 3,148 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-Aerozine-50
${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.04
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,563
Reference Velocity (exhaust m / s)
1,627
Chamber Temperature (K)
3,148
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-Aerozine-50 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.04 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,563 Reference Velocity (exhaust m / s) 1,627 Chamber Temperature (K) 3,148 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-Aerozine-50
${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.04
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,563
Reference Velocity (exhaust m / s)
1,627
Chamber Temperature (K)
3,148
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-Aerozine-50 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.04 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,563 Reference Velocity (exhaust m / s) 1,627 Chamber Temperature (K) 3,148 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-Aerozine-50
${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.04
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,563
Reference Velocity (exhaust m / s)
1,627
Chamber Temperature (K)
3,148
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-Aerozine-50 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.04 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,563 Reference Velocity (exhaust m / s) 1,627 Chamber Temperature (K) 3,148 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-Ammonia
${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
3.58
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
261
Effective Velocity (exhaust m / s)
2,453
Reference Velocity (exhaust m / s)
1,552
Chamber Temperature (K)
2,842
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.04
| NO-Ammonia ${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 3.58 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 261 Effective Velocity (exhaust m / s) 2,453 Reference Velocity (exhaust m / s) 1,552 Chamber Temperature (K) 2,842 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.04 |
NO-Ammonia
${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
3.58
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
261
Effective Velocity (exhaust m / s)
2,453
Reference Velocity (exhaust m / s)
1,552
Chamber Temperature (K)
2,842
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.04
| NO-Ammonia ${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 3.58 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 261 Effective Velocity (exhaust m / s) 2,453 Reference Velocity (exhaust m / s) 1,552 Chamber Temperature (K) 2,842 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.04 |
NO-Ammonia
${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
3.58
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
261
Effective Velocity (exhaust m / s)
2,453
Reference Velocity (exhaust m / s)
1,552
Chamber Temperature (K)
2,842
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.04
| NO-Ammonia ${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 3.58 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 261 Effective Velocity (exhaust m / s) 2,453 Reference Velocity (exhaust m / s) 1,552 Chamber Temperature (K) 2,842 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.04 |
NO-Ammonia
${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
3.58
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
261
Effective Velocity (exhaust m / s)
2,453
Reference Velocity (exhaust m / s)
1,552
Chamber Temperature (K)
2,842
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.04
| NO-Ammonia ${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 3.58 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 261 Effective Velocity (exhaust m / s) 2,453 Reference Velocity (exhaust m / s) 1,552 Chamber Temperature (K) 2,842 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.04 |
NO-Ammonia
${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
3.58
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
261
Effective Velocity (exhaust m / s)
2,453
Reference Velocity (exhaust m / s)
1,552
Chamber Temperature (K)
2,842
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.04
| NO-Ammonia ${ N }_{ 2 }{ O }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 3.58 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 261 Effective Velocity (exhaust m / s) 2,453 Reference Velocity (exhaust m / s) 1,552 Chamber Temperature (K) 2,842 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.04 |
NO-Aniline
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
5.26
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,415
Reference Velocity (exhaust m / s)
1,536
Chamber Temperature (K)
3,321
Exhaust Weight (g / mole)
27.10
Specific Heat Ratio (gamma)
1.25
Propellant Density (kg / l)
1.19
| NO-Aniline ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 5.26 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,415 Reference Velocity (exhaust m / s) 1,536 Chamber Temperature (K) 3,321 Exhaust Weight (g / mole) 27.10 Specific Heat Ratio (gamma) 1.25 Propellant Density (kg / l) 1.19 |
NO-Aniline
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
5.26
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,415
Reference Velocity (exhaust m / s)
1,536
Chamber Temperature (K)
3,321
Exhaust Weight (g / mole)
27.10
Specific Heat Ratio (gamma)
1.25
Propellant Density (kg / l)
1.19
| NO-Aniline ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 5.26 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,415 Reference Velocity (exhaust m / s) 1,536 Chamber Temperature (K) 3,321 Exhaust Weight (g / mole) 27.10 Specific Heat Ratio (gamma) 1.25 Propellant Density (kg / l) 1.19 |
NO-Aniline
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
5.26
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,415
Reference Velocity (exhaust m / s)
1,536
Chamber Temperature (K)
3,321
Exhaust Weight (g / mole)
27.10
Specific Heat Ratio (gamma)
1.25
Propellant Density (kg / l)
1.19
| NO-Aniline ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 5.26 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,415 Reference Velocity (exhaust m / s) 1,536 Chamber Temperature (K) 3,321 Exhaust Weight (g / mole) 27.10 Specific Heat Ratio (gamma) 1.25 Propellant Density (kg / l) 1.19 |
NO-Aniline
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
5.26
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,415
Reference Velocity (exhaust m / s)
1,536
Chamber Temperature (K)
3,321
Exhaust Weight (g / mole)
27.10
Specific Heat Ratio (gamma)
1.25
Propellant Density (kg / l)
1.19
| NO-Aniline ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 5.26 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,415 Reference Velocity (exhaust m / s) 1,536 Chamber Temperature (K) 3,321 Exhaust Weight (g / mole) 27.10 Specific Heat Ratio (gamma) 1.25 Propellant Density (kg / l) 1.19 |
NO-Aniline
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
5.26
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,415
Reference Velocity (exhaust m / s)
1,536
Chamber Temperature (K)
3,321
Exhaust Weight (g / mole)
27.10
Specific Heat Ratio (gamma)
1.25
Propellant Density (kg / l)
1.19
| NO-Aniline ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 5.26 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,415 Reference Velocity (exhaust m / s) 1,536 Chamber Temperature (K) 3,321 Exhaust Weight (g / mole) 27.10 Specific Heat Ratio (gamma) 1.25 Propellant Density (kg / l) 1.19 |
NO-Ethanol-75
${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.70
Specific Impulse (seconds @ sl)
241
Density Impulse (kg · s · l @ sl)
268
Effective Velocity (exhaust m / s)
2,367
Reference Velocity (exhaust m / s)
1,494
Chamber Temperature (K)
2,957
Exhaust Weight (g / mole)
25.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.11
| NO-Ethanol-75 ${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.70 Specific Impulse (seconds @ sl) 241 Density Impulse (kg · s · l @ sl) 268 Effective Velocity (exhaust m / s) 2,367 Reference Velocity (exhaust m / s) 1,494 Chamber Temperature (K) 2,957 Exhaust Weight (g / mole) 25.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.11 |
NO-Ethanol-75
${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.70
Specific Impulse (seconds @ sl)
241
Density Impulse (kg · s · l @ sl)
268
Effective Velocity (exhaust m / s)
2,367
Reference Velocity (exhaust m / s)
1,494
Chamber Temperature (K)
2,957
Exhaust Weight (g / mole)
25.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.11
| NO-Ethanol-75 ${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.70 Specific Impulse (seconds @ sl) 241 Density Impulse (kg · s · l @ sl) 268 Effective Velocity (exhaust m / s) 2,367 Reference Velocity (exhaust m / s) 1,494 Chamber Temperature (K) 2,957 Exhaust Weight (g / mole) 25.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.11 |
NO-Ethanol-75
${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.70
Specific Impulse (seconds @ sl)
241
Density Impulse (kg · s · l @ sl)
268
Effective Velocity (exhaust m / s)
2,367
Reference Velocity (exhaust m / s)
1,494
Chamber Temperature (K)
2,957
Exhaust Weight (g / mole)
25.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.11
| NO-Ethanol-75 ${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.70 Specific Impulse (seconds @ sl) 241 Density Impulse (kg · s · l @ sl) 268 Effective Velocity (exhaust m / s) 2,367 Reference Velocity (exhaust m / s) 1,494 Chamber Temperature (K) 2,957 Exhaust Weight (g / mole) 25.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.11 |
NO-Ethanol-75
${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.70
Specific Impulse (seconds @ sl)
241
Density Impulse (kg · s · l @ sl)
268
Effective Velocity (exhaust m / s)
2,367
Reference Velocity (exhaust m / s)
1,494
Chamber Temperature (K)
2,957
Exhaust Weight (g / mole)
25.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.11
| NO-Ethanol-75 ${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.70 Specific Impulse (seconds @ sl) 241 Density Impulse (kg · s · l @ sl) 268 Effective Velocity (exhaust m / s) 2,367 Reference Velocity (exhaust m / s) 1,494 Chamber Temperature (K) 2,957 Exhaust Weight (g / mole) 25.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.11 |
NO-Ethanol-75
${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
3.70
Specific Impulse (seconds @ sl)
241
Density Impulse (kg · s · l @ sl)
268
Effective Velocity (exhaust m / s)
2,367
Reference Velocity (exhaust m / s)
1,494
Chamber Temperature (K)
2,957
Exhaust Weight (g / mole)
25.90
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.11
| NO-Ethanol-75 ${ N }_{ 2 }{ O }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 3.70 Specific Impulse (seconds @ sl) 241 Density Impulse (kg · s · l @ sl) 268 Effective Velocity (exhaust m / s) 2,367 Reference Velocity (exhaust m / s) 1,494 Chamber Temperature (K) 2,957 Exhaust Weight (g / mole) 25.90 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.11 |
NO-Ethanol-95
${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ethanol (75%) Water (25%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
4.37
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
273
Effective Velocity (exhaust m / s)
2,408
Reference Velocity (exhaust m / s)
1,523
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
25.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.11
| NO-Ethanol-95 ${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ethanol (75%) Water (25%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 4.37 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 273 Effective Velocity (exhaust m / s) 2,408 Reference Velocity (exhaust m / s) 1,523 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 25.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.11 |
NO-Ethanol-95
${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ethanol (75%) Water (25%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
4.37
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
273
Effective Velocity (exhaust m / s)
2,408
Reference Velocity (exhaust m / s)
1,523
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
25.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.11
| NO-Ethanol-95 ${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ethanol (75%) Water (25%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 4.37 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 273 Effective Velocity (exhaust m / s) 2,408 Reference Velocity (exhaust m / s) 1,523 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 25.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.11 |
NO-Ethanol-95
${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ethanol (75%) Water (25%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
4.37
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
273
Effective Velocity (exhaust m / s)
2,408
Reference Velocity (exhaust m / s)
1,523
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
25.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.11
| NO-Ethanol-95 ${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ethanol (75%) Water (25%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 4.37 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 273 Effective Velocity (exhaust m / s) 2,408 Reference Velocity (exhaust m / s) 1,523 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 25.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.11 |
NO-Ethanol-95
${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ethanol (75%) Water (25%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
4.37
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
273
Effective Velocity (exhaust m / s)
2,408
Reference Velocity (exhaust m / s)
1,523
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
25.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.11
| NO-Ethanol-95 ${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ethanol (75%) Water (25%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 4.37 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 273 Effective Velocity (exhaust m / s) 2,408 Reference Velocity (exhaust m / s) 1,523 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 25.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.11 |
NO-Ethanol-95
${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Ethanol (75%) Water (25%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43.657’84
Mixture Ratio (X:1)
4.37
Specific Impulse (seconds @ sl)
246
Density Impulse (kg · s · l @ sl)
273
Effective Velocity (exhaust m / s)
2,408
Reference Velocity (exhaust m / s)
1,523
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
25.80
Specific Heat Ratio (gamma)
1.23
Propellant Density (kg / l)
1.11
| NO-Ethanol-95 ${ N }_{ 2 }{ O }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Ethanol (75%) Water (25%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43.657’84 Mixture Ratio (X:1) 4.37 Specific Impulse (seconds @ sl) 246 Density Impulse (kg · s · l @ sl) 273 Effective Velocity (exhaust m / s) 2,408 Reference Velocity (exhaust m / s) 1,523 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 25.80 Specific Heat Ratio (gamma) 1.23 Propellant Density (kg / l) 1.11 |
NO-HTPB
${ N }_{ 2 }{ O }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
6.48
Specific Impulse (seconds @ sl)
248
Density Impulse (kg · s · l @ sl)
290
Effective Velocity (exhaust m / s)
2,429
Reference Velocity (exhaust m / s)
1,544
Chamber Temperature (K)
3,286
Exhaust Weight (g / mole)
26.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.17
| NO-HTPB ${ N }_{ 2 }{ O }$ ⋅ HTPB Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 6.48 Specific Impulse (seconds @ sl) 248 Density Impulse (kg · s · l @ sl) 290 Effective Velocity (exhaust m / s) 2,429 Reference Velocity (exhaust m / s) 1,544 Chamber Temperature (K) 3,286 Exhaust Weight (g / mole) 26.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.17 |
NO-HTPB
${ N }_{ 2 }{ O }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
6.48
Specific Impulse (seconds @ sl)
248
Density Impulse (kg · s · l @ sl)
290
Effective Velocity (exhaust m / s)
2,429
Reference Velocity (exhaust m / s)
1,544
Chamber Temperature (K)
3,286
Exhaust Weight (g / mole)
26.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.17
| NO-HTPB ${ N }_{ 2 }{ O }$ ⋅ HTPB Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 6.48 Specific Impulse (seconds @ sl) 248 Density Impulse (kg · s · l @ sl) 290 Effective Velocity (exhaust m / s) 2,429 Reference Velocity (exhaust m / s) 1,544 Chamber Temperature (K) 3,286 Exhaust Weight (g / mole) 26.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.17 |
NO-HTPB
${ N }_{ 2 }{ O }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
6.48
Specific Impulse (seconds @ sl)
248
Density Impulse (kg · s · l @ sl)
290
Effective Velocity (exhaust m / s)
2,429
Reference Velocity (exhaust m / s)
1,544
Chamber Temperature (K)
3,286
Exhaust Weight (g / mole)
26.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.17
| NO-HTPB ${ N }_{ 2 }{ O }$ ⋅ HTPB Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 6.48 Specific Impulse (seconds @ sl) 248 Density Impulse (kg · s · l @ sl) 290 Effective Velocity (exhaust m / s) 2,429 Reference Velocity (exhaust m / s) 1,544 Chamber Temperature (K) 3,286 Exhaust Weight (g / mole) 26.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.17 |
NO-HTPB
${ N }_{ 2 }{ O }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
6.48
Specific Impulse (seconds @ sl)
248
Density Impulse (kg · s · l @ sl)
290
Effective Velocity (exhaust m / s)
2,429
Reference Velocity (exhaust m / s)
1,544
Chamber Temperature (K)
3,286
Exhaust Weight (g / mole)
26.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.17
| NO-HTPB ${ N }_{ 2 }{ O }$ ⋅ HTPB Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 6.48 Specific Impulse (seconds @ sl) 248 Density Impulse (kg · s · l @ sl) 290 Effective Velocity (exhaust m / s) 2,429 Reference Velocity (exhaust m / s) 1,544 Chamber Temperature (K) 3,286 Exhaust Weight (g / mole) 26.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.17 |
NO-HTPB
${ N }_{ 2 }{ O }$ ⋅ HTPB
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
6.48
Specific Impulse (seconds @ sl)
248
Density Impulse (kg · s · l @ sl)
290
Effective Velocity (exhaust m / s)
2,429
Reference Velocity (exhaust m / s)
1,544
Chamber Temperature (K)
3,286
Exhaust Weight (g / mole)
26.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.17
| NO-HTPB ${ N }_{ 2 }{ O }$ ⋅ HTPB Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 6.48 Specific Impulse (seconds @ sl) 248 Density Impulse (kg · s · l @ sl) 290 Effective Velocity (exhaust m / s) 2,429 Reference Velocity (exhaust m / s) 1,544 Chamber Temperature (K) 3,286 Exhaust Weight (g / mole) 26.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.17 |
NO-Hydrazine
${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.96
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
304
Effective Velocity (exhaust m / s)
2,620
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,042
Exhaust Weight (g / mole)
21.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.14
| NO-Hydrazine ${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.96 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 304 Effective Velocity (exhaust m / s) 2,620 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,042 Exhaust Weight (g / mole) 21.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.14 |
NO-Hydrazine
${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.96
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
304
Effective Velocity (exhaust m / s)
2,620
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,042
Exhaust Weight (g / mole)
21.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.14
| NO-Hydrazine ${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.96 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 304 Effective Velocity (exhaust m / s) 2,620 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,042 Exhaust Weight (g / mole) 21.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.14 |
NO-Hydrazine
${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.96
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
304
Effective Velocity (exhaust m / s)
2,620
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,042
Exhaust Weight (g / mole)
21.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.14
| NO-Hydrazine ${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.96 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 304 Effective Velocity (exhaust m / s) 2,620 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,042 Exhaust Weight (g / mole) 21.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.14 |
NO-Hydrazine
${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.96
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
304
Effective Velocity (exhaust m / s)
2,620
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,042
Exhaust Weight (g / mole)
21.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.14
| NO-Hydrazine ${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.96 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 304 Effective Velocity (exhaust m / s) 2,620 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,042 Exhaust Weight (g / mole) 21.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.14 |
NO-Hydrazine
${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.96
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
304
Effective Velocity (exhaust m / s)
2,620
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,042
Exhaust Weight (g / mole)
21.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.14
| NO-Hydrazine ${ N }_{ 2 }{ O }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.96 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 304 Effective Velocity (exhaust m / s) 2,620 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,042 Exhaust Weight (g / mole) 21.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.14 |
NO-Hydrogen
${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
12.00
Specific Impulse (seconds @ sl)
294
Density Impulse (kg · s · l @ sl)
160
Effective Velocity (exhaust m / s)
2,883
Reference Velocity (exhaust m / s)
1,828
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
16.80
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
0.54
| NO-Hydrogen ${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 12.00 Specific Impulse (seconds @ sl) 294 Density Impulse (kg · s · l @ sl) 160 Effective Velocity (exhaust m / s) 2,883 Reference Velocity (exhaust m / s) 1,828 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 16.80 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 0.54 |
NO-Hydrogen
${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
12.00
Specific Impulse (seconds @ sl)
294
Density Impulse (kg · s · l @ sl)
160
Effective Velocity (exhaust m / s)
2,883
Reference Velocity (exhaust m / s)
1,828
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
16.80
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
0.54
| NO-Hydrogen ${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 12.00 Specific Impulse (seconds @ sl) 294 Density Impulse (kg · s · l @ sl) 160 Effective Velocity (exhaust m / s) 2,883 Reference Velocity (exhaust m / s) 1,828 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 16.80 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 0.54 |
NO-Hydrogen
${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
12.00
Specific Impulse (seconds @ sl)
294
Density Impulse (kg · s · l @ sl)
160
Effective Velocity (exhaust m / s)
2,883
Reference Velocity (exhaust m / s)
1,828
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
16.80
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
0.54
| NO-Hydrogen ${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 12.00 Specific Impulse (seconds @ sl) 294 Density Impulse (kg · s · l @ sl) 160 Effective Velocity (exhaust m / s) 2,883 Reference Velocity (exhaust m / s) 1,828 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 16.80 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 0.54 |
NO-Hydrogen
${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
12.00
Specific Impulse (seconds @ sl)
294
Density Impulse (kg · s · l @ sl)
160
Effective Velocity (exhaust m / s)
2,883
Reference Velocity (exhaust m / s)
1,828
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
16.80
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
0.54
| NO-Hydrogen ${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 12.00 Specific Impulse (seconds @ sl) 294 Density Impulse (kg · s · l @ sl) 160 Effective Velocity (exhaust m / s) 2,883 Reference Velocity (exhaust m / s) 1,828 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 16.80 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 0.54 |
NO-Hydrogen
${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
12.00
Specific Impulse (seconds @ sl)
294
Density Impulse (kg · s · l @ sl)
160
Effective Velocity (exhaust m / s)
2,883
Reference Velocity (exhaust m / s)
1,828
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
16.80
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
0.54
| NO-Hydrogen ${ N }_{ 2 }{ O }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 12.00 Specific Impulse (seconds @ sl) 294 Density Impulse (kg · s · l @ sl) 160 Effective Velocity (exhaust m / s) 2,883 Reference Velocity (exhaust m / s) 1,828 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 16.80 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 0.54 |
NO-Kerosene
${ N }_{ 2 }{ O }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
7.01
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,455
Reference Velocity (exhaust m / s)
1,559
Chamber Temperature (K)
3,241
Exhaust Weight (g / mole)
25.70
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Kerosene ${ N }_{ 2 }{ O }$ ⋅ RP-1 Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 7.01 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,455 Reference Velocity (exhaust m / s) 1,559 Chamber Temperature (K) 3,241 Exhaust Weight (g / mole) 25.70 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Kerosene
${ N }_{ 2 }{ O }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
7.01
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,455
Reference Velocity (exhaust m / s)
1,559
Chamber Temperature (K)
3,241
Exhaust Weight (g / mole)
25.70
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Kerosene ${ N }_{ 2 }{ O }$ ⋅ RP-1 Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 7.01 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,455 Reference Velocity (exhaust m / s) 1,559 Chamber Temperature (K) 3,241 Exhaust Weight (g / mole) 25.70 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Kerosene
${ N }_{ 2 }{ O }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
7.01
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,455
Reference Velocity (exhaust m / s)
1,559
Chamber Temperature (K)
3,241
Exhaust Weight (g / mole)
25.70
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Kerosene ${ N }_{ 2 }{ O }$ ⋅ RP-1 Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 7.01 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,455 Reference Velocity (exhaust m / s) 1,559 Chamber Temperature (K) 3,241 Exhaust Weight (g / mole) 25.70 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Kerosene
${ N }_{ 2 }{ O }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
7.01
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,455
Reference Velocity (exhaust m / s)
1,559
Chamber Temperature (K)
3,241
Exhaust Weight (g / mole)
25.70
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Kerosene ${ N }_{ 2 }{ O }$ ⋅ RP-1 Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 7.01 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,455 Reference Velocity (exhaust m / s) 1,559 Chamber Temperature (K) 3,241 Exhaust Weight (g / mole) 25.70 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Kerosene
${ N }_{ 2 }{ O }$ ⋅ RP-1
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
7.01
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
288
Effective Velocity (exhaust m / s)
2,455
Reference Velocity (exhaust m / s)
1,559
Chamber Temperature (K)
3,241
Exhaust Weight (g / mole)
25.70
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Kerosene ${ N }_{ 2 }{ O }$ ⋅ RP-1 Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 7.01 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 288 Effective Velocity (exhaust m / s) 2,455 Reference Velocity (exhaust m / s) 1,559 Chamber Temperature (K) 3,241 Exhaust Weight (g / mole) 25.70 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Methane
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
8.42
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
258
Effective Velocity (exhaust m / s)
2,485
Reference Velocity (exhaust m / s)
1,575
Chamber Temperature (K)
3,147
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.02
| NO-Methane ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 8.42 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 258 Effective Velocity (exhaust m / s) 2,485 Reference Velocity (exhaust m / s) 1,575 Chamber Temperature (K) 3,147 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.02 |
NO-Methane
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
8.42
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
258
Effective Velocity (exhaust m / s)
2,485
Reference Velocity (exhaust m / s)
1,575
Chamber Temperature (K)
3,147
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.02
| NO-Methane ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 8.42 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 258 Effective Velocity (exhaust m / s) 2,485 Reference Velocity (exhaust m / s) 1,575 Chamber Temperature (K) 3,147 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.02 |
NO-Methane
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
8.42
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
258
Effective Velocity (exhaust m / s)
2,485
Reference Velocity (exhaust m / s)
1,575
Chamber Temperature (K)
3,147
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.02
| NO-Methane ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 8.42 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 258 Effective Velocity (exhaust m / s) 2,485 Reference Velocity (exhaust m / s) 1,575 Chamber Temperature (K) 3,147 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.02 |
NO-Methane
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
8.42
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
258
Effective Velocity (exhaust m / s)
2,485
Reference Velocity (exhaust m / s)
1,575
Chamber Temperature (K)
3,147
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.02
| NO-Methane ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 8.42 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 258 Effective Velocity (exhaust m / s) 2,485 Reference Velocity (exhaust m / s) 1,575 Chamber Temperature (K) 3,147 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.02 |
NO-Methane
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
8.42
Specific Impulse (seconds @ sl)
253
Density Impulse (kg · s · l @ sl)
258
Effective Velocity (exhaust m / s)
2,485
Reference Velocity (exhaust m / s)
1,575
Chamber Temperature (K)
3,147
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.02
| NO-Methane ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 8.42 Specific Impulse (seconds @ sl) 253 Density Impulse (kg · s · l @ sl) 258 Effective Velocity (exhaust m / s) 2,485 Reference Velocity (exhaust m / s) 1,575 Chamber Temperature (K) 3,147 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.02 |
NO-Methanol
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
3.40
Specific Impulse (seconds @ sl)
245
Density Impulse (kg · s · l @ sl)
267
Effective Velocity (exhaust m / s)
2,404
Reference Velocity (exhaust m / s)
1,517
Chamber Temperature (K)
2,998
Exhaust Weight (g / mole)
25.40
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.09
| NO-Methanol ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 3.40 Specific Impulse (seconds @ sl) 245 Density Impulse (kg · s · l @ sl) 267 Effective Velocity (exhaust m / s) 2,404 Reference Velocity (exhaust m / s) 1,517 Chamber Temperature (K) 2,998 Exhaust Weight (g / mole) 25.40 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.09 |
NO-Methanol
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
3.40
Specific Impulse (seconds @ sl)
245
Density Impulse (kg · s · l @ sl)
267
Effective Velocity (exhaust m / s)
2,404
Reference Velocity (exhaust m / s)
1,517
Chamber Temperature (K)
2,998
Exhaust Weight (g / mole)
25.40
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.09
| NO-Methanol ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 3.40 Specific Impulse (seconds @ sl) 245 Density Impulse (kg · s · l @ sl) 267 Effective Velocity (exhaust m / s) 2,404 Reference Velocity (exhaust m / s) 1,517 Chamber Temperature (K) 2,998 Exhaust Weight (g / mole) 25.40 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.09 |
NO-Methanol
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
3.40
Specific Impulse (seconds @ sl)
245
Density Impulse (kg · s · l @ sl)
267
Effective Velocity (exhaust m / s)
2,404
Reference Velocity (exhaust m / s)
1,517
Chamber Temperature (K)
2,998
Exhaust Weight (g / mole)
25.40
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.09
| NO-Methanol ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 3.40 Specific Impulse (seconds @ sl) 245 Density Impulse (kg · s · l @ sl) 267 Effective Velocity (exhaust m / s) 2,404 Reference Velocity (exhaust m / s) 1,517 Chamber Temperature (K) 2,998 Exhaust Weight (g / mole) 25.40 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.09 |
NO-Methanol
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
3.40
Specific Impulse (seconds @ sl)
245
Density Impulse (kg · s · l @ sl)
267
Effective Velocity (exhaust m / s)
2,404
Reference Velocity (exhaust m / s)
1,517
Chamber Temperature (K)
2,998
Exhaust Weight (g / mole)
25.40
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.09
| NO-Methanol ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 3.40 Specific Impulse (seconds @ sl) 245 Density Impulse (kg · s · l @ sl) 267 Effective Velocity (exhaust m / s) 2,404 Reference Velocity (exhaust m / s) 1,517 Chamber Temperature (K) 2,998 Exhaust Weight (g / mole) 25.40 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.09 |
NO-Methanol
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
3.40
Specific Impulse (seconds @ sl)
245
Density Impulse (kg · s · l @ sl)
267
Effective Velocity (exhaust m / s)
2,404
Reference Velocity (exhaust m / s)
1,517
Chamber Temperature (K)
2,998
Exhaust Weight (g / mole)
25.40
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.09
| NO-Methanol ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 3.40 Specific Impulse (seconds @ sl) 245 Density Impulse (kg · s · l @ sl) 267 Effective Velocity (exhaust m / s) 2,404 Reference Velocity (exhaust m / s) 1,517 Chamber Temperature (K) 2,998 Exhaust Weight (g / mole) 25.40 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.09 |
NO-MMH
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
3.34
Specific Impulse (seconds @ sl)
260
Density Impulse (kg · s · l @ sl)
291
Effective Velocity (exhaust m / s)
2,554
Reference Velocity (exhaust m / s)
1,622
Chamber Temperature (K)
3,171
Exhaust Weight (g / mole)
23.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-MMH ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 3.34 Specific Impulse (seconds @ sl) 260 Density Impulse (kg · s · l @ sl) 291 Effective Velocity (exhaust m / s) 2,554 Reference Velocity (exhaust m / s) 1,622 Chamber Temperature (K) 3,171 Exhaust Weight (g / mole) 23.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-MMH
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
3.34
Specific Impulse (seconds @ sl)
260
Density Impulse (kg · s · l @ sl)
291
Effective Velocity (exhaust m / s)
2,554
Reference Velocity (exhaust m / s)
1,622
Chamber Temperature (K)
3,171
Exhaust Weight (g / mole)
23.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-MMH ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 3.34 Specific Impulse (seconds @ sl) 260 Density Impulse (kg · s · l @ sl) 291 Effective Velocity (exhaust m / s) 2,554 Reference Velocity (exhaust m / s) 1,622 Chamber Temperature (K) 3,171 Exhaust Weight (g / mole) 23.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-MMH
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
3.34
Specific Impulse (seconds @ sl)
260
Density Impulse (kg · s · l @ sl)
291
Effective Velocity (exhaust m / s)
2,554
Reference Velocity (exhaust m / s)
1,622
Chamber Temperature (K)
3,171
Exhaust Weight (g / mole)
23.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-MMH ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 3.34 Specific Impulse (seconds @ sl) 260 Density Impulse (kg · s · l @ sl) 291 Effective Velocity (exhaust m / s) 2,554 Reference Velocity (exhaust m / s) 1,622 Chamber Temperature (K) 3,171 Exhaust Weight (g / mole) 23.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-MMH
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
3.34
Specific Impulse (seconds @ sl)
260
Density Impulse (kg · s · l @ sl)
291
Effective Velocity (exhaust m / s)
2,554
Reference Velocity (exhaust m / s)
1,622
Chamber Temperature (K)
3,171
Exhaust Weight (g / mole)
23.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-MMH ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 3.34 Specific Impulse (seconds @ sl) 260 Density Impulse (kg · s · l @ sl) 291 Effective Velocity (exhaust m / s) 2,554 Reference Velocity (exhaust m / s) 1,622 Chamber Temperature (K) 3,171 Exhaust Weight (g / mole) 23.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-MMH
${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
3.34
Specific Impulse (seconds @ sl)
260
Density Impulse (kg · s · l @ sl)
291
Effective Velocity (exhaust m / s)
2,554
Reference Velocity (exhaust m / s)
1,622
Chamber Temperature (K)
3,171
Exhaust Weight (g / mole)
23.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.12
| NO-MMH ${ N }_{ 2 }{ O }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 3.34 Specific Impulse (seconds @ sl) 260 Density Impulse (kg · s · l @ sl) 291 Effective Velocity (exhaust m / s) 2,554 Reference Velocity (exhaust m / s) 1,622 Chamber Temperature (K) 3,171 Exhaust Weight (g / mole) 23.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.12 |
NO-Tonka-250
${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
6.02
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,438
Reference Velocity (exhaust m / s)
1,548
Chamber Temperature (K)
3,253
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Tonka-250 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 6.02 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,438 Reference Velocity (exhaust m / s) 1,548 Chamber Temperature (K) 3,253 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Tonka-250
${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
6.02
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,438
Reference Velocity (exhaust m / s)
1,548
Chamber Temperature (K)
3,253
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Tonka-250 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 6.02 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,438 Reference Velocity (exhaust m / s) 1,548 Chamber Temperature (K) 3,253 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Tonka-250
${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
6.02
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,438
Reference Velocity (exhaust m / s)
1,548
Chamber Temperature (K)
3,253
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Tonka-250 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 6.02 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,438 Reference Velocity (exhaust m / s) 1,548 Chamber Temperature (K) 3,253 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Tonka-250
${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
6.02
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,438
Reference Velocity (exhaust m / s)
1,548
Chamber Temperature (K)
3,253
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Tonka-250 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 6.02 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,438 Reference Velocity (exhaust m / s) 1,548 Chamber Temperature (K) 3,253 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-Tonka-250
${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
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)
6.02
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,438
Reference Velocity (exhaust m / s)
1,548
Chamber Temperature (K)
3,253
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.15
| NO-Tonka-250 ${ N }_{ 2 }{ O }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 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) 6.02 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,438 Reference Velocity (exhaust m / s) 1,548 Chamber Temperature (K) 3,253 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.15 |
NO-UDMH
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
4.10
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,209
Exhaust Weight (g / mole)
24.00
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.10-
| NO-UDMH ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 4.10 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,209 Exhaust Weight (g / mole) 24.00 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.10- |
NO-UDMH
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
4.10
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,209
Exhaust Weight (g / mole)
24.00
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.10-
| NO-UDMH ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 4.10 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,209 Exhaust Weight (g / mole) 24.00 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.10- |
NO-UDMH
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
4.10
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,209
Exhaust Weight (g / mole)
24.00
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.10-
| NO-UDMH ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 4.10 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,209 Exhaust Weight (g / mole) 24.00 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.10- |
NO-UDMH
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
4.10
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,209
Exhaust Weight (g / mole)
24.00
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.10-
| NO-UDMH ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 4.10 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,209 Exhaust Weight (g / mole) 24.00 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.10- |
NO-UDMH
${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Nitrous Oxide
${ N }_{ 2 }{ O }$
Molecular Weight (Oxidiser)
44.012’80
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
4.10
Specific Impulse (seconds @ sl)
258
Density Impulse (kg · s · l @ sl)
285
Effective Velocity (exhaust m / s)
2,528
Reference Velocity (exhaust m / s)
1,606
Chamber Temperature (K)
3,209
Exhaust Weight (g / mole)
24.00
Specific Heat Ratio (gamma)
1.24
Propellant Density (kg / l)
1.10-
| NO-UDMH ${ N }_{ 2 }{ O }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Nitrous Oxide ${ N }_{ 2 }{ O }$ Molecular Weight (Oxidiser) 44.012’80 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 4.10 Specific Impulse (seconds @ sl) 258 Density Impulse (kg · s · l @ sl) 285 Effective Velocity (exhaust m / s) 2,528 Reference Velocity (exhaust m / s) 1,606 Chamber Temperature (K) 3,209 Exhaust Weight (g / mole) 24.00 Specific Heat Ratio (gamma) 1.24 Propellant Density (kg / l) 1.10- |