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
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOx, Fluorine + Oxygen
FLOX-Aerozine-25
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.480’27
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)
2.41
Specific Impulse (seconds @ sl)
332
Density Impulse (kg · s · l @ sl)
411
Effective Velocity (exhaust m / s)
3,255
Reference Velocity (exhaust m / s)
2,104
Chamber Temperature (K)
4,584
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.24
| FLOX-Aerozine-25 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.480’27 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) 2.41 Specific Impulse (seconds @ sl) 332 Density Impulse (kg · s · l @ sl) 411 Effective Velocity (exhaust m / s) 3,255 Reference Velocity (exhaust m / s) 2,104 Chamber Temperature (K) 4,584 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.24 |
FLOX-Aerozine-25
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.480’27
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)
2.41
Specific Impulse (seconds @ sl)
332
Density Impulse (kg · s · l @ sl)
411
Effective Velocity (exhaust m / s)
3,255
Reference Velocity (exhaust m / s)
2,104
Chamber Temperature (K)
4,584
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.24
| FLOX-Aerozine-25 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.480’27 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) 2.41 Specific Impulse (seconds @ sl) 332 Density Impulse (kg · s · l @ sl) 411 Effective Velocity (exhaust m / s) 3,255 Reference Velocity (exhaust m / s) 2,104 Chamber Temperature (K) 4,584 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.24 |
FLOX-Aerozine-25
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.480’27
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)
2.41
Specific Impulse (seconds @ sl)
332
Density Impulse (kg · s · l @ sl)
411
Effective Velocity (exhaust m / s)
3,255
Reference Velocity (exhaust m / s)
2,104
Chamber Temperature (K)
4,584
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.24
| FLOX-Aerozine-25 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.480’27 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) 2.41 Specific Impulse (seconds @ sl) 332 Density Impulse (kg · s · l @ sl) 411 Effective Velocity (exhaust m / s) 3,255 Reference Velocity (exhaust m / s) 2,104 Chamber Temperature (K) 4,584 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.24 |
FLOX-Aerozine-25
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.480’27
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)
2.41
Specific Impulse (seconds @ sl)
332
Density Impulse (kg · s · l @ sl)
411
Effective Velocity (exhaust m / s)
3,255
Reference Velocity (exhaust m / s)
2,104
Chamber Temperature (K)
4,584
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.24
| FLOX-Aerozine-25 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.480’27 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) 2.41 Specific Impulse (seconds @ sl) 332 Density Impulse (kg · s · l @ sl) 411 Effective Velocity (exhaust m / s) 3,255 Reference Velocity (exhaust m / s) 2,104 Chamber Temperature (K) 4,584 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.24 |
FLOX-Aerozine-25
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.480’27
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)
2.41
Specific Impulse (seconds @ sl)
332
Density Impulse (kg · s · l @ sl)
411
Effective Velocity (exhaust m / s)
3,255
Reference Velocity (exhaust m / s)
2,104
Chamber Temperature (K)
4,584
Exhaust Weight (g / mole)
19.30
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.24
| FLOX-Aerozine-25 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 83% (${ F }_{ 2 }$) + 17% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.480’27 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) 2.41 Specific Impulse (seconds @ sl) 332 Density Impulse (kg · s · l @ sl) 411 Effective Velocity (exhaust m / s) 3,255 Reference Velocity (exhaust m / s) 2,104 Chamber Temperature (K) 4,584 Exhaust Weight (g / mole) 19.30 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.24 |
FLOX-Aerozine-50
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.629’72
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)
2.22
Specific Impulse (seconds @ sl)
334
Density Impulse (kg · s · l @ sl)
403
Effective Velocity (exhaust m / s)
3,273
Reference Velocity (exhaust m / s)
2,115
Chamber Temperature (K)
4,575
Exhaust Weight (g / mole)
19.00
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.21
| FLOX-Aerozine-50 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.629’72 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) 2.22 Specific Impulse (seconds @ sl) 334 Density Impulse (kg · s · l @ sl) 403 Effective Velocity (exhaust m / s) 3,273 Reference Velocity (exhaust m / s) 2,115 Chamber Temperature (K) 4,575 Exhaust Weight (g / mole) 19.00 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.21 |
FLOX-Aerozine-50
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.629’72
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)
2.22
Specific Impulse (seconds @ sl)
334
Density Impulse (kg · s · l @ sl)
403
Effective Velocity (exhaust m / s)
3,273
Reference Velocity (exhaust m / s)
2,115
Chamber Temperature (K)
4,575
Exhaust Weight (g / mole)
19.00
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.21
| FLOX-Aerozine-50 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.629’72 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) 2.22 Specific Impulse (seconds @ sl) 334 Density Impulse (kg · s · l @ sl) 403 Effective Velocity (exhaust m / s) 3,273 Reference Velocity (exhaust m / s) 2,115 Chamber Temperature (K) 4,575 Exhaust Weight (g / mole) 19.00 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.21 |
FLOX-Aerozine-50
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.629’72
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)
2.22
Specific Impulse (seconds @ sl)
334
Density Impulse (kg · s · l @ sl)
403
Effective Velocity (exhaust m / s)
3,273
Reference Velocity (exhaust m / s)
2,115
Chamber Temperature (K)
4,575
Exhaust Weight (g / mole)
19.00
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.21
| FLOX-Aerozine-50 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.629’72 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) 2.22 Specific Impulse (seconds @ sl) 334 Density Impulse (kg · s · l @ sl) 403 Effective Velocity (exhaust m / s) 3,273 Reference Velocity (exhaust m / s) 2,115 Chamber Temperature (K) 4,575 Exhaust Weight (g / mole) 19.00 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.21 |
FLOX-Aerozine-50
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.629’72
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)
2.22
Specific Impulse (seconds @ sl)
334
Density Impulse (kg · s · l @ sl)
403
Effective Velocity (exhaust m / s)
3,273
Reference Velocity (exhaust m / s)
2,115
Chamber Temperature (K)
4,575
Exhaust Weight (g / mole)
19.00
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.21
| FLOX-Aerozine-50 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.629’72 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) 2.22 Specific Impulse (seconds @ sl) 334 Density Impulse (kg · s · l @ sl) 403 Effective Velocity (exhaust m / s) 3,273 Reference Velocity (exhaust m / s) 2,115 Chamber Temperature (K) 4,575 Exhaust Weight (g / mole) 19.00 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.21 |
FLOX-Aerozine-50
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Fluorine + Oxygen
88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.629’72
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)
2.22
Specific Impulse (seconds @ sl)
334
Density Impulse (kg · s · l @ sl)
403
Effective Velocity (exhaust m / s)
3,273
Reference Velocity (exhaust m / s)
2,115
Chamber Temperature (K)
4,575
Exhaust Weight (g / mole)
19.00
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.21
| FLOX-Aerozine-50 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Fluorine + Oxygen 88% (${ F }_{ 2 }$) + 12% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.629’72 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) 2.22 Specific Impulse (seconds @ sl) 334 Density Impulse (kg · s · l @ sl) 403 Effective Velocity (exhaust m / s) 3,273 Reference Velocity (exhaust m / s) 2,115 Chamber Temperature (K) 4,575 Exhaust Weight (g / mole) 19.00 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.21 |
FLOX-Aniline
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Oxidiser (Liquid)
Fluorine + Oxygen
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17.703’13
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.41
Specific Impulse (seconds @ sl)
306
Density Impulse (kg · s · l @ sl)
373
Effective Velocity (exhaust m / s)
3,006
Reference Velocity (exhaust m / s)
1,939
Chamber Temperature (K)
4,517
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.22
| FLOX-Aniline 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Oxidiser (Liquid) Fluorine + Oxygen 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17.703’13 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.41 Specific Impulse (seconds @ sl) 306 Density Impulse (kg · s · l @ sl) 373 Effective Velocity (exhaust m / s) 3,006 Reference Velocity (exhaust m / s) 1,939 Chamber Temperature (K) 4,517 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.22 |
FLOX-Aniline
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Oxidiser (Liquid)
Fluorine + Oxygen
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17.703’13
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.41
Specific Impulse (seconds @ sl)
306
Density Impulse (kg · s · l @ sl)
373
Effective Velocity (exhaust m / s)
3,006
Reference Velocity (exhaust m / s)
1,939
Chamber Temperature (K)
4,517
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.22
| FLOX-Aniline 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Oxidiser (Liquid) Fluorine + Oxygen 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17.703’13 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.41 Specific Impulse (seconds @ sl) 306 Density Impulse (kg · s · l @ sl) 373 Effective Velocity (exhaust m / s) 3,006 Reference Velocity (exhaust m / s) 1,939 Chamber Temperature (K) 4,517 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.22 |
FLOX-Aniline
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Oxidiser (Liquid)
Fluorine + Oxygen
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17.703’13
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.41
Specific Impulse (seconds @ sl)
306
Density Impulse (kg · s · l @ sl)
373
Effective Velocity (exhaust m / s)
3,006
Reference Velocity (exhaust m / s)
1,939
Chamber Temperature (K)
4,517
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.22
| FLOX-Aniline 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Oxidiser (Liquid) Fluorine + Oxygen 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17.703’13 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.41 Specific Impulse (seconds @ sl) 306 Density Impulse (kg · s · l @ sl) 373 Effective Velocity (exhaust m / s) 3,006 Reference Velocity (exhaust m / s) 1,939 Chamber Temperature (K) 4,517 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.22 |
FLOX-Aniline
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Oxidiser (Liquid)
Fluorine + Oxygen
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17.703’13
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.41
Specific Impulse (seconds @ sl)
306
Density Impulse (kg · s · l @ sl)
373
Effective Velocity (exhaust m / s)
3,006
Reference Velocity (exhaust m / s)
1,939
Chamber Temperature (K)
4,517
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.22
| FLOX-Aniline 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Oxidiser (Liquid) Fluorine + Oxygen 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17.703’13 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.41 Specific Impulse (seconds @ sl) 306 Density Impulse (kg · s · l @ sl) 373 Effective Velocity (exhaust m / s) 3,006 Reference Velocity (exhaust m / s) 1,939 Chamber Temperature (K) 4,517 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.22 |
FLOX-Aniline
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Oxidiser (Liquid)
Fluorine + Oxygen
57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17.703’13
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
2.41
Specific Impulse (seconds @ sl)
306
Density Impulse (kg · s · l @ sl)
373
Effective Velocity (exhaust m / s)
3,006
Reference Velocity (exhaust m / s)
1,939
Chamber Temperature (K)
4,517
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.22
| FLOX-Aniline 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Oxidiser (Liquid) Fluorine + Oxygen 57% (${ F }_{ 2 }$) + 43% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17.703’13 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{2}$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 2.41 Specific Impulse (seconds @ sl) 306 Density Impulse (kg · s · l @ sl) 373 Effective Velocity (exhaust m / s) 3,006 Reference Velocity (exhaust m / s) 1,939 Chamber Temperature (K) 4,517 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.22 |
FLOX-Ethanol-95
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Fluorine + Oxygen
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.659’61
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43,657’84
Mixture Ratio (X:1)
2.56
Specific Impulse (seconds @ sl)
320
Density Impulse (kg · s · l @ sl)
377
Effective Velocity (exhaust m / s)
3,134
Reference Velocity (exhaust m / s)
2,023
Chamber Temperature (K)
4,437
Exhaust Weight (g / mole)
20.20
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Ethanol-95 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Fluorine + Oxygen 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.659’61 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43,657’84 Mixture Ratio (X:1) 2.56 Specific Impulse (seconds @ sl) 320 Density Impulse (kg · s · l @ sl) 377 Effective Velocity (exhaust m / s) 3,134 Reference Velocity (exhaust m / s) 2,023 Chamber Temperature (K) 4,437 Exhaust Weight (g / mole) 20.20 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Ethanol-95
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Fluorine + Oxygen
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.659’61
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43,657’84
Mixture Ratio (X:1)
2.56
Specific Impulse (seconds @ sl)
320
Density Impulse (kg · s · l @ sl)
377
Effective Velocity (exhaust m / s)
3,134
Reference Velocity (exhaust m / s)
2,023
Chamber Temperature (K)
4,437
Exhaust Weight (g / mole)
20.20
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Ethanol-95 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Fluorine + Oxygen 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.659’61 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43,657’84 Mixture Ratio (X:1) 2.56 Specific Impulse (seconds @ sl) 320 Density Impulse (kg · s · l @ sl) 377 Effective Velocity (exhaust m / s) 3,134 Reference Velocity (exhaust m / s) 2,023 Chamber Temperature (K) 4,437 Exhaust Weight (g / mole) 20.20 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Ethanol-95
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Fluorine + Oxygen
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.659’61
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43,657’84
Mixture Ratio (X:1)
2.56
Specific Impulse (seconds @ sl)
320
Density Impulse (kg · s · l @ sl)
377
Effective Velocity (exhaust m / s)
3,134
Reference Velocity (exhaust m / s)
2,023
Chamber Temperature (K)
4,437
Exhaust Weight (g / mole)
20.20
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Ethanol-95 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Fluorine + Oxygen 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.659’61 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43,657’84 Mixture Ratio (X:1) 2.56 Specific Impulse (seconds @ sl) 320 Density Impulse (kg · s · l @ sl) 377 Effective Velocity (exhaust m / s) 3,134 Reference Velocity (exhaust m / s) 2,023 Chamber Temperature (K) 4,437 Exhaust Weight (g / mole) 20.20 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Ethanol-95
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Fluorine + Oxygen
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.659’61
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43,657’84
Mixture Ratio (X:1)
2.56
Specific Impulse (seconds @ sl)
320
Density Impulse (kg · s · l @ sl)
377
Effective Velocity (exhaust m / s)
3,134
Reference Velocity (exhaust m / s)
2,023
Chamber Temperature (K)
4,437
Exhaust Weight (g / mole)
20.20
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Ethanol-95 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Fluorine + Oxygen 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.659’61 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43,657’84 Mixture Ratio (X:1) 2.56 Specific Impulse (seconds @ sl) 320 Density Impulse (kg · s · l @ sl) 377 Effective Velocity (exhaust m / s) 3,134 Reference Velocity (exhaust m / s) 2,023 Chamber Temperature (K) 4,437 Exhaust Weight (g / mole) 20.20 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Ethanol-95
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Fluorine + Oxygen
89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18.659’61
Fuel (Liquid)
Ethanol (95%) Water (5%)
95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Molecular Weight (Fuel)
43,657’84
Mixture Ratio (X:1)
2.56
Specific Impulse (seconds @ sl)
320
Density Impulse (kg · s · l @ sl)
377
Effective Velocity (exhaust m / s)
3,134
Reference Velocity (exhaust m / s)
2,023
Chamber Temperature (K)
4,437
Exhaust Weight (g / mole)
20.20
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Ethanol-95 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Fluorine + Oxygen 89% (${ F }_{ 2 }$) + 11% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18.659’61 Fuel (Liquid) Ethanol (95%) Water (5%) 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Molecular Weight (Fuel) 43,657’84 Mixture Ratio (X:1) 2.56 Specific Impulse (seconds @ sl) 320 Density Impulse (kg · s · l @ sl) 377 Effective Velocity (exhaust m / s) 3,134 Reference Velocity (exhaust m / s) 2,023 Chamber Temperature (K) 4,437 Exhaust Weight (g / mole) 20.20 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-HTPB
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB
Oxidiser (Liquid)
Fluorine + Oxygen
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17,852’58
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
3.14
Specific Impulse (seconds @ sl)
314
Density Impulse (kg · s · l @ sl)
380
Effective Velocity (exhaust m / s)
3,082
Reference Velocity (exhaust m / s)
1,990
Chamber Temperature (K)
4,555
Exhaust Weight (g / mole)
21.50
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.21
| FLOX-HTPB 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB Oxidiser (Liquid) Fluorine + Oxygen 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17,852’58 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 3.14 Specific Impulse (seconds @ sl) 314 Density Impulse (kg · s · l @ sl) 380 Effective Velocity (exhaust m / s) 3,082 Reference Velocity (exhaust m / s) 1,990 Chamber Temperature (K) 4,555 Exhaust Weight (g / mole) 21.50 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.21 |
FLOX-HTPB
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB
Oxidiser (Liquid)
Fluorine + Oxygen
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17,852’58
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
3.14
Specific Impulse (seconds @ sl)
314
Density Impulse (kg · s · l @ sl)
380
Effective Velocity (exhaust m / s)
3,082
Reference Velocity (exhaust m / s)
1,990
Chamber Temperature (K)
4,555
Exhaust Weight (g / mole)
21.50
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.21
| FLOX-HTPB 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB Oxidiser (Liquid) Fluorine + Oxygen 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17,852’58 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 3.14 Specific Impulse (seconds @ sl) 314 Density Impulse (kg · s · l @ sl) 380 Effective Velocity (exhaust m / s) 3,082 Reference Velocity (exhaust m / s) 1,990 Chamber Temperature (K) 4,555 Exhaust Weight (g / mole) 21.50 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.21 |
FLOX-HTPB
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB
Oxidiser (Liquid)
Fluorine + Oxygen
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17,852’58
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
3.14
Specific Impulse (seconds @ sl)
314
Density Impulse (kg · s · l @ sl)
380
Effective Velocity (exhaust m / s)
3,082
Reference Velocity (exhaust m / s)
1,990
Chamber Temperature (K)
4,555
Exhaust Weight (g / mole)
21.50
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.21
| FLOX-HTPB 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB Oxidiser (Liquid) Fluorine + Oxygen 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17,852’58 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 3.14 Specific Impulse (seconds @ sl) 314 Density Impulse (kg · s · l @ sl) 380 Effective Velocity (exhaust m / s) 3,082 Reference Velocity (exhaust m / s) 1,990 Chamber Temperature (K) 4,555 Exhaust Weight (g / mole) 21.50 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.21 |
FLOX-HTPB
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB
Oxidiser (Liquid)
Fluorine + Oxygen
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17,852’58
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
3.14
Specific Impulse (seconds @ sl)
314
Density Impulse (kg · s · l @ sl)
380
Effective Velocity (exhaust m / s)
3,082
Reference Velocity (exhaust m / s)
1,990
Chamber Temperature (K)
4,555
Exhaust Weight (g / mole)
21.50
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.21
| FLOX-HTPB 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB Oxidiser (Liquid) Fluorine + Oxygen 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17,852’58 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 3.14 Specific Impulse (seconds @ sl) 314 Density Impulse (kg · s · l @ sl) 380 Effective Velocity (exhaust m / s) 3,082 Reference Velocity (exhaust m / s) 1,990 Chamber Temperature (K) 4,555 Exhaust Weight (g / mole) 21.50 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.21 |
FLOX-HTPB
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB
Oxidiser (Liquid)
Fluorine + Oxygen
62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
17,852’58
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’05
Mixture Ratio (X:1)
3.14
Specific Impulse (seconds @ sl)
314
Density Impulse (kg · s · l @ sl)
380
Effective Velocity (exhaust m / s)
3,082
Reference Velocity (exhaust m / s)
1,990
Chamber Temperature (K)
4,555
Exhaust Weight (g / mole)
21.50
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.21
| FLOX-HTPB 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) ⋅ HTPB Oxidiser (Liquid) Fluorine + Oxygen 62% (${ F }_{ 2 }$) + 38% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 17,852’58 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’05 Mixture Ratio (X:1) 3.14 Specific Impulse (seconds @ sl) 314 Density Impulse (kg · s · l @ sl) 380 Effective Velocity (exhaust m / s) 3,082 Reference Velocity (exhaust m / s) 1,990 Chamber Temperature (K) 4,555 Exhaust Weight (g / mole) 21.50 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.21 |
FLOX-Kerosene
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1
Oxidiser (Liquid)
Fluorine + Oxygen
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,061’81
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.67
Specific Impulse (seconds @ sl)
323
Density Impulse (kg · s · l @ sl)
386
Effective Velocity (exhaust m / s)
3,166
Reference Velocity (exhaust m / s)
2,045
Chamber Temperature (K)
4,571
Exhaust Weight (g / mole)
20.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.19
| FLOX-Kerosene 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1 Oxidiser (Liquid) Fluorine + Oxygen 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,061’81 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.67 Specific Impulse (seconds @ sl) 323 Density Impulse (kg · s · l @ sl) 386 Effective Velocity (exhaust m / s) 3,166 Reference Velocity (exhaust m / s) 2,045 Chamber Temperature (K) 4,571 Exhaust Weight (g / mole) 20.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.19 |
FLOX-Kerosene
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1
Oxidiser (Liquid)
Fluorine + Oxygen
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,061’81
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.67
Specific Impulse (seconds @ sl)
323
Density Impulse (kg · s · l @ sl)
386
Effective Velocity (exhaust m / s)
3,166
Reference Velocity (exhaust m / s)
2,045
Chamber Temperature (K)
4,571
Exhaust Weight (g / mole)
20.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.19
| FLOX-Kerosene 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1 Oxidiser (Liquid) Fluorine + Oxygen 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,061’81 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.67 Specific Impulse (seconds @ sl) 323 Density Impulse (kg · s · l @ sl) 386 Effective Velocity (exhaust m / s) 3,166 Reference Velocity (exhaust m / s) 2,045 Chamber Temperature (K) 4,571 Exhaust Weight (g / mole) 20.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.19 |
FLOX-Kerosene
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1
Oxidiser (Liquid)
Fluorine + Oxygen
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,061’81
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.67
Specific Impulse (seconds @ sl)
323
Density Impulse (kg · s · l @ sl)
386
Effective Velocity (exhaust m / s)
3,166
Reference Velocity (exhaust m / s)
2,045
Chamber Temperature (K)
4,571
Exhaust Weight (g / mole)
20.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.19
| FLOX-Kerosene 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1 Oxidiser (Liquid) Fluorine + Oxygen 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,061’81 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.67 Specific Impulse (seconds @ sl) 323 Density Impulse (kg · s · l @ sl) 386 Effective Velocity (exhaust m / s) 3,166 Reference Velocity (exhaust m / s) 2,045 Chamber Temperature (K) 4,571 Exhaust Weight (g / mole) 20.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.19 |
FLOX-Kerosene
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1
Oxidiser (Liquid)
Fluorine + Oxygen
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,061’81
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.67
Specific Impulse (seconds @ sl)
323
Density Impulse (kg · s · l @ sl)
386
Effective Velocity (exhaust m / s)
3,166
Reference Velocity (exhaust m / s)
2,045
Chamber Temperature (K)
4,571
Exhaust Weight (g / mole)
20.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.19
| FLOX-Kerosene 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1 Oxidiser (Liquid) Fluorine + Oxygen 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,061’81 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.67 Specific Impulse (seconds @ sl) 323 Density Impulse (kg · s · l @ sl) 386 Effective Velocity (exhaust m / s) 3,166 Reference Velocity (exhaust m / s) 2,045 Chamber Temperature (K) 4,571 Exhaust Weight (g / mole) 20.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.19 |
FLOX-Kerosene
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1
Oxidiser (Liquid)
Fluorine + Oxygen
69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,061’81
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’18
Mixture Ratio (X:1)
3.67
Specific Impulse (seconds @ sl)
323
Density Impulse (kg · s · l @ sl)
386
Effective Velocity (exhaust m / s)
3,166
Reference Velocity (exhaust m / s)
2,045
Chamber Temperature (K)
4,571
Exhaust Weight (g / mole)
20.40
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.19
| FLOX-Kerosene 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) ⋅ RP-1 Oxidiser (Liquid) Fluorine + Oxygen 69% (${ F }_{ 2 }$) + 31% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,061’81 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’18 Mixture Ratio (X:1) 3.67 Specific Impulse (seconds @ sl) 323 Density Impulse (kg · s · l @ sl) 386 Effective Velocity (exhaust m / s) 3,166 Reference Velocity (exhaust m / s) 2,045 Chamber Temperature (K) 4,571 Exhaust Weight (g / mole) 20.40 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.19 |
FLOX-Methane
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Fluorine + Oxygen
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,360’71
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16,042’46
Mixture Ratio (X:1)
4.82
Specific Impulse (seconds @ sl)
335
Density Impulse (kg · s · l @ sl)
337
Effective Velocity (exhaust m / s)
3,281
Reference Velocity (exhaust m / s)
2,120
Chamber Temperature (K)
4,530
Exhaust Weight (g / mole)
18.80
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.01
| FLOX-Methane 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Fluorine + Oxygen 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,360’71 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16,042’46 Mixture Ratio (X:1) 4.82 Specific Impulse (seconds @ sl) 335 Density Impulse (kg · s · l @ sl) 337 Effective Velocity (exhaust m / s) 3,281 Reference Velocity (exhaust m / s) 2,120 Chamber Temperature (K) 4,530 Exhaust Weight (g / mole) 18.80 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.01 |
FLOX-Methane
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Fluorine + Oxygen
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,360’71
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16,042’46
Mixture Ratio (X:1)
4.82
Specific Impulse (seconds @ sl)
335
Density Impulse (kg · s · l @ sl)
337
Effective Velocity (exhaust m / s)
3,281
Reference Velocity (exhaust m / s)
2,120
Chamber Temperature (K)
4,530
Exhaust Weight (g / mole)
18.80
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.01
| FLOX-Methane 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Fluorine + Oxygen 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,360’71 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16,042’46 Mixture Ratio (X:1) 4.82 Specific Impulse (seconds @ sl) 335 Density Impulse (kg · s · l @ sl) 337 Effective Velocity (exhaust m / s) 3,281 Reference Velocity (exhaust m / s) 2,120 Chamber Temperature (K) 4,530 Exhaust Weight (g / mole) 18.80 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.01 |
FLOX-Methane
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Fluorine + Oxygen
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,360’71
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16,042’46
Mixture Ratio (X:1)
4.82
Specific Impulse (seconds @ sl)
335
Density Impulse (kg · s · l @ sl)
337
Effective Velocity (exhaust m / s)
3,281
Reference Velocity (exhaust m / s)
2,120
Chamber Temperature (K)
4,530
Exhaust Weight (g / mole)
18.80
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.01
| FLOX-Methane 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Fluorine + Oxygen 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,360’71 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16,042’46 Mixture Ratio (X:1) 4.82 Specific Impulse (seconds @ sl) 335 Density Impulse (kg · s · l @ sl) 337 Effective Velocity (exhaust m / s) 3,281 Reference Velocity (exhaust m / s) 2,120 Chamber Temperature (K) 4,530 Exhaust Weight (g / mole) 18.80 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.01 |
FLOX-Methane
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Fluorine + Oxygen
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,360’71
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16,042’46
Mixture Ratio (X:1)
4.82
Specific Impulse (seconds @ sl)
335
Density Impulse (kg · s · l @ sl)
337
Effective Velocity (exhaust m / s)
3,281
Reference Velocity (exhaust m / s)
2,120
Chamber Temperature (K)
4,530
Exhaust Weight (g / mole)
18.80
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.01
| FLOX-Methane 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Fluorine + Oxygen 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,360’71 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16,042’46 Mixture Ratio (X:1) 4.82 Specific Impulse (seconds @ sl) 335 Density Impulse (kg · s · l @ sl) 337 Effective Velocity (exhaust m / s) 3,281 Reference Velocity (exhaust m / s) 2,120 Chamber Temperature (K) 4,530 Exhaust Weight (g / mole) 18.80 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.01 |
FLOX-Methane
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Fluorine + Oxygen
79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,360’71
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16,042’46
Mixture Ratio (X:1)
4.82
Specific Impulse (seconds @ sl)
335
Density Impulse (kg · s · l @ sl)
337
Effective Velocity (exhaust m / s)
3,281
Reference Velocity (exhaust m / s)
2,120
Chamber Temperature (K)
4,530
Exhaust Weight (g / mole)
18.80
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.01
| FLOX-Methane 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Fluorine + Oxygen 79% (${ F }_{ 2 }$) + 21% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,360’71 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16,042’46 Mixture Ratio (X:1) 4.82 Specific Impulse (seconds @ sl) 335 Density Impulse (kg · s · l @ sl) 337 Effective Velocity (exhaust m / s) 3,281 Reference Velocity (exhaust m / s) 2,120 Chamber Temperature (K) 4,530 Exhaust Weight (g / mole) 18.80 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.01 |
FLOX-MMH
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,540’05
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.33
Specific Impulse (seconds @ sl)
333
Density Impulse (kg · s · l @ sl)
399
Effective Velocity (exhaust m / s)
3,264
Reference Velocity (exhaust m / s)
2,110
Chamber Temperature (K)
4,583
Exhaust Weight (g / mole)
19.20
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.20
| FLOX-MMH 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,540’05 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.33 Specific Impulse (seconds @ sl) 333 Density Impulse (kg · s · l @ sl) 399 Effective Velocity (exhaust m / s) 3,264 Reference Velocity (exhaust m / s) 2,110 Chamber Temperature (K) 4,583 Exhaust Weight (g / mole) 19.20 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.20 |
FLOX-MMH
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,540’05
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.33
Specific Impulse (seconds @ sl)
333
Density Impulse (kg · s · l @ sl)
399
Effective Velocity (exhaust m / s)
3,264
Reference Velocity (exhaust m / s)
2,110
Chamber Temperature (K)
4,583
Exhaust Weight (g / mole)
19.20
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.20
| FLOX-MMH 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,540’05 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.33 Specific Impulse (seconds @ sl) 333 Density Impulse (kg · s · l @ sl) 399 Effective Velocity (exhaust m / s) 3,264 Reference Velocity (exhaust m / s) 2,110 Chamber Temperature (K) 4,583 Exhaust Weight (g / mole) 19.20 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.20 |
FLOX-MMH
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,540’05
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.33
Specific Impulse (seconds @ sl)
333
Density Impulse (kg · s · l @ sl)
399
Effective Velocity (exhaust m / s)
3,264
Reference Velocity (exhaust m / s)
2,110
Chamber Temperature (K)
4,583
Exhaust Weight (g / mole)
19.20
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.20
| FLOX-MMH 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,540’05 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.33 Specific Impulse (seconds @ sl) 333 Density Impulse (kg · s · l @ sl) 399 Effective Velocity (exhaust m / s) 3,264 Reference Velocity (exhaust m / s) 2,110 Chamber Temperature (K) 4,583 Exhaust Weight (g / mole) 19.20 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.20 |
FLOX-MMH
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,540’05
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.33
Specific Impulse (seconds @ sl)
333
Density Impulse (kg · s · l @ sl)
399
Effective Velocity (exhaust m / s)
3,264
Reference Velocity (exhaust m / s)
2,110
Chamber Temperature (K)
4,583
Exhaust Weight (g / mole)
19.20
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.20
| FLOX-MMH 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,540’05 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.33 Specific Impulse (seconds @ sl) 333 Density Impulse (kg · s · l @ sl) 399 Effective Velocity (exhaust m / s) 3,264 Reference Velocity (exhaust m / s) 2,110 Chamber Temperature (K) 4,583 Exhaust Weight (g / mole) 19.20 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.20 |
FLOX-MMH
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,540’05
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.33
Specific Impulse (seconds @ sl)
333
Density Impulse (kg · s · l @ sl)
399
Effective Velocity (exhaust m / s)
3,264
Reference Velocity (exhaust m / s)
2,110
Chamber Temperature (K)
4,583
Exhaust Weight (g / mole)
19.20
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.20
| FLOX-MMH 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 85% (${ F }_{ 2 }$) + 15% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,540’05 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.33 Specific Impulse (seconds @ sl) 333 Density Impulse (kg · s · l @ sl) 399 Effective Velocity (exhaust m / s) 3,264 Reference Velocity (exhaust m / s) 2,110 Chamber Temperature (K) 4,583 Exhaust Weight (g / mole) 19.20 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.20 |
FLOX-Tonka-250
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Fluorine + Oxygen
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,002’03
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.07
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
374
Effective Velocity (exhaust m / s)
3,114
Reference Velocity (exhaust m / s)
2,010
Chamber Temperature (K)
4,553
Exhaust Weight (g / mole)
21.00
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Tonka-250 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Fluorine + Oxygen 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,002’03 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.07 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 374 Effective Velocity (exhaust m / s) 3,114 Reference Velocity (exhaust m / s) 2,010 Chamber Temperature (K) 4,553 Exhaust Weight (g / mole) 21.00 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Tonka-250
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Fluorine + Oxygen
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,002’03
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.07
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
374
Effective Velocity (exhaust m / s)
3,114
Reference Velocity (exhaust m / s)
2,010
Chamber Temperature (K)
4,553
Exhaust Weight (g / mole)
21.00
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Tonka-250 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Fluorine + Oxygen 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,002’03 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.07 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 374 Effective Velocity (exhaust m / s) 3,114 Reference Velocity (exhaust m / s) 2,010 Chamber Temperature (K) 4,553 Exhaust Weight (g / mole) 21.00 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Tonka-250
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Fluorine + Oxygen
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,002’03
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.07
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
374
Effective Velocity (exhaust m / s)
3,114
Reference Velocity (exhaust m / s)
2,010
Chamber Temperature (K)
4,553
Exhaust Weight (g / mole)
21.00
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Tonka-250 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Fluorine + Oxygen 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,002’03 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.07 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 374 Effective Velocity (exhaust m / s) 3,114 Reference Velocity (exhaust m / s) 2,010 Chamber Temperature (K) 4,553 Exhaust Weight (g / mole) 21.00 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Tonka-250
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Fluorine + Oxygen
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,002’03
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.07
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
374
Effective Velocity (exhaust m / s)
3,114
Reference Velocity (exhaust m / s)
2,010
Chamber Temperature (K)
4,553
Exhaust Weight (g / mole)
21.00
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Tonka-250 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Fluorine + Oxygen 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,002’03 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.07 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 374 Effective Velocity (exhaust m / s) 3,114 Reference Velocity (exhaust m / s) 2,010 Chamber Temperature (K) 4,553 Exhaust Weight (g / mole) 21.00 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-Tonka-250
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Fluorine + Oxygen
67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,002’03
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.07
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
374
Effective Velocity (exhaust m / s)
3,114
Reference Velocity (exhaust m / s)
2,010
Chamber Temperature (K)
4,553
Exhaust Weight (g / mole)
21.00
Specific Heat Ratio (gamma)
1.30
Propellant Density (kg / l)
1.18
| FLOX-Tonka-250 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) ⋅ 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Fluorine + Oxygen 67% (${ F }_{ 2 }$) + 33% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,002’03 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ CH }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.07 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 374 Effective Velocity (exhaust m / s) 3,114 Reference Velocity (exhaust m / s) 2,010 Chamber Temperature (K) 4,553 Exhaust Weight (g / mole) 21.00 Specific Heat Ratio (gamma) 1.30 Propellant Density (kg / l) 1.18 |
FLOX-UDMH
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,390’60
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.60
Specific Impulse (seconds @ sl)
330
Density Impulse (kg · s · l @ sl)
383
Effective Velocity (exhaust m / s)
3,239
Reference Velocity (exhaust m / s)
2,093
Chamber Temperature (K)
4,591
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.16
| FLOX-UDMH 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,390’60 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.60 Specific Impulse (seconds @ sl) 330 Density Impulse (kg · s · l @ sl) 383 Effective Velocity (exhaust m / s) 3,239 Reference Velocity (exhaust m / s) 2,093 Chamber Temperature (K) 4,591 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.16 |
FLOX-UDMH
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,390’60
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.60
Specific Impulse (seconds @ sl)
330
Density Impulse (kg · s · l @ sl)
383
Effective Velocity (exhaust m / s)
3,239
Reference Velocity (exhaust m / s)
2,093
Chamber Temperature (K)
4,591
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.16
| FLOX-UDMH 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,390’60 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.60 Specific Impulse (seconds @ sl) 330 Density Impulse (kg · s · l @ sl) 383 Effective Velocity (exhaust m / s) 3,239 Reference Velocity (exhaust m / s) 2,093 Chamber Temperature (K) 4,591 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.16 |
FLOX-UDMH
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,390’60
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.60
Specific Impulse (seconds @ sl)
330
Density Impulse (kg · s · l @ sl)
383
Effective Velocity (exhaust m / s)
3,239
Reference Velocity (exhaust m / s)
2,093
Chamber Temperature (K)
4,591
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.16
| FLOX-UDMH 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,390’60 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.60 Specific Impulse (seconds @ sl) 330 Density Impulse (kg · s · l @ sl) 383 Effective Velocity (exhaust m / s) 3,239 Reference Velocity (exhaust m / s) 2,093 Chamber Temperature (K) 4,591 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.16 |
FLOX-UDMH
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,390’60
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.60
Specific Impulse (seconds @ sl)
330
Density Impulse (kg · s · l @ sl)
383
Effective Velocity (exhaust m / s)
3,239
Reference Velocity (exhaust m / s)
2,093
Chamber Temperature (K)
4,591
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.16
| FLOX-UDMH 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,390’60 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.60 Specific Impulse (seconds @ sl) 330 Density Impulse (kg · s · l @ sl) 383 Effective Velocity (exhaust m / s) 3,239 Reference Velocity (exhaust m / s) 2,093 Chamber Temperature (K) 4,591 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.16 |
FLOX-UDMH
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Fluorine + Oxygen
80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$)
Molecular Weight (Oxidiser)
18,390’60
Fuel (Liquid)
Unsymmetrical Dimethylhydrazine
${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Molecular Weight (Fuel)
60.098’32
Mixture Ratio (X:1)
2.60
Specific Impulse (seconds @ sl)
330
Density Impulse (kg · s · l @ sl)
383
Effective Velocity (exhaust m / s)
3,239
Reference Velocity (exhaust m / s)
2,093
Chamber Temperature (K)
4,591
Exhaust Weight (g / mole)
19.50
Specific Heat Ratio (gamma)
1.31
Propellant Density (kg / l)
1.16
| FLOX-UDMH 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Fluorine + Oxygen 80% (${ F }_{ 2 }$) + 20% (${ O }_{ 2 }$) Molecular Weight (Oxidiser) 18,390’60 Fuel (Liquid) Unsymmetrical Dimethylhydrazine ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Molecular Weight (Fuel) 60.098’32 Mixture Ratio (X:1) 2.60 Specific Impulse (seconds @ sl) 330 Density Impulse (kg · s · l @ sl) 383 Effective Velocity (exhaust m / s) 3,239 Reference Velocity (exhaust m / s) 2,093 Chamber Temperature (K) 4,591 Exhaust Weight (g / mole) 19.50 Specific Heat Ratio (gamma) 1.31 Propellant Density (kg / l) 1.16 |