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
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA, Red Fuming Nitric Acid
RFNA-Aerozine-25
${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.27
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
324
Effective Velocity (exhaust m / s)
2,622
Reference Velocity (exhaust m / s)
1,649
Chamber Temperature (K)
3,037
Exhaust Weight (g / mole)
21.90
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-Aerozine-25 ${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.27 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 324 Effective Velocity (exhaust m / s) 2,622 Reference Velocity (exhaust m / s) 1,649 Chamber Temperature (K) 3,037 Exhaust Weight (g / mole) 21.90 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-Aerozine-25
${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.27
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
324
Effective Velocity (exhaust m / s)
2,622
Reference Velocity (exhaust m / s)
1,649
Chamber Temperature (K)
3,037
Exhaust Weight (g / mole)
21.90
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-Aerozine-25 ${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.27 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 324 Effective Velocity (exhaust m / s) 2,622 Reference Velocity (exhaust m / s) 1,649 Chamber Temperature (K) 3,037 Exhaust Weight (g / mole) 21.90 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-Aerozine-25
${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.27
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
324
Effective Velocity (exhaust m / s)
2,622
Reference Velocity (exhaust m / s)
1,649
Chamber Temperature (K)
3,037
Exhaust Weight (g / mole)
21.90
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-Aerozine-25 ${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.27 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 324 Effective Velocity (exhaust m / s) 2,622 Reference Velocity (exhaust m / s) 1,649 Chamber Temperature (K) 3,037 Exhaust Weight (g / mole) 21.90 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-Aerozine-25
${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.27
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
324
Effective Velocity (exhaust m / s)
2,622
Reference Velocity (exhaust m / s)
1,649
Chamber Temperature (K)
3,037
Exhaust Weight (g / mole)
21.90
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-Aerozine-25 ${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.27 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 324 Effective Velocity (exhaust m / s) 2,622 Reference Velocity (exhaust m / s) 1,649 Chamber Temperature (K) 3,037 Exhaust Weight (g / mole) 21.90 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-Aerozine-25
${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.27
Specific Impulse (seconds @ sl)
267
Density Impulse (kg · s · l @ sl)
324
Effective Velocity (exhaust m / s)
2,622
Reference Velocity (exhaust m / s)
1,649
Chamber Temperature (K)
3,037
Exhaust Weight (g / mole)
21.90
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-Aerozine-25 ${ HNO }_{ 3 }$ ⋅ 25% (${ N }_{ 2 }{ H }_{ 4 }$) + 75% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.27 Specific Impulse (seconds @ sl) 267 Density Impulse (kg · s · l @ sl) 324 Effective Velocity (exhaust m / s) 2,622 Reference Velocity (exhaust m / s) 1,649 Chamber Temperature (K) 3,037 Exhaust Weight (g / mole) 21.90 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-Aerozine-50
${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.94
Specific Impulse (seconds @ sl)
270
Density Impulse (kg · s · l @ sl)
329
Effective Velocity (exhaust m / s)
2,643
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,009
Exhaust Weight (g / mole)
21.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-Aerozine-50 ${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.94 Specific Impulse (seconds @ sl) 270 Density Impulse (kg · s · l @ sl) 329 Effective Velocity (exhaust m / s) 2,643 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,009 Exhaust Weight (g / mole) 21.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-Aerozine-50
${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.94
Specific Impulse (seconds @ sl)
270
Density Impulse (kg · s · l @ sl)
329
Effective Velocity (exhaust m / s)
2,643
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,009
Exhaust Weight (g / mole)
21.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-Aerozine-50 ${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.94 Specific Impulse (seconds @ sl) 270 Density Impulse (kg · s · l @ sl) 329 Effective Velocity (exhaust m / s) 2,643 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,009 Exhaust Weight (g / mole) 21.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-Aerozine-50
${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.94
Specific Impulse (seconds @ sl)
270
Density Impulse (kg · s · l @ sl)
329
Effective Velocity (exhaust m / s)
2,643
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,009
Exhaust Weight (g / mole)
21.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-Aerozine-50 ${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.94 Specific Impulse (seconds @ sl) 270 Density Impulse (kg · s · l @ sl) 329 Effective Velocity (exhaust m / s) 2,643 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,009 Exhaust Weight (g / mole) 21.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-Aerozine-50
${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.94
Specific Impulse (seconds @ sl)
270
Density Impulse (kg · s · l @ sl)
329
Effective Velocity (exhaust m / s)
2,643
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,009
Exhaust Weight (g / mole)
21.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-Aerozine-50 ${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.94 Specific Impulse (seconds @ sl) 270 Density Impulse (kg · s · l @ sl) 329 Effective Velocity (exhaust m / s) 2,643 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,009 Exhaust Weight (g / mole) 21.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-Aerozine-50
${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrazine (50%) UDMH (50%)
50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$)
Molecular Weight (Fuel)
46.071’83
Mixture Ratio (X:1)
1.94
Specific Impulse (seconds @ sl)
270
Density Impulse (kg · s · l @ sl)
329
Effective Velocity (exhaust m / s)
2,643
Reference Velocity (exhaust m / s)
1,663
Chamber Temperature (K)
3,009
Exhaust Weight (g / mole)
21.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-Aerozine-50 ${ HNO }_{ 3 }$ ⋅ 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrazine (50%) UDMH (50%) 50% (${ N }_{ 2 }{ H }_{ 4 }$) + 50% (${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$) Molecular Weight (Fuel) 46.071’83 Mixture Ratio (X:1) 1.94 Specific Impulse (seconds @ sl) 270 Density Impulse (kg · s · l @ sl) 329 Effective Velocity (exhaust m / s) 2,643 Reference Velocity (exhaust m / s) 1,663 Chamber Temperature (K) 3,009 Exhaust Weight (g / mole) 21.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-Ammonia
${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
2.18
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,487
Reference Velocity (exhaust m / s)
1,562
Chamber Temperature (K)
2,572
Exhaust Weight (g / mole)
20.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.09
| RFNA-Ammonia ${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 2.18 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,487 Reference Velocity (exhaust m / s) 1,562 Chamber Temperature (K) 2,572 Exhaust Weight (g / mole) 20.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.09 |
RFNA-Ammonia
${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
2.18
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,487
Reference Velocity (exhaust m / s)
1,562
Chamber Temperature (K)
2,572
Exhaust Weight (g / mole)
20.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.09
| RFNA-Ammonia ${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 2.18 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,487 Reference Velocity (exhaust m / s) 1,562 Chamber Temperature (K) 2,572 Exhaust Weight (g / mole) 20.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.09 |
RFNA-Ammonia
${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
2.18
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,487
Reference Velocity (exhaust m / s)
1,562
Chamber Temperature (K)
2,572
Exhaust Weight (g / mole)
20.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.09
| RFNA-Ammonia ${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 2.18 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,487 Reference Velocity (exhaust m / s) 1,562 Chamber Temperature (K) 2,572 Exhaust Weight (g / mole) 20.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.09 |
RFNA-Ammonia
${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
2.18
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,487
Reference Velocity (exhaust m / s)
1,562
Chamber Temperature (K)
2,572
Exhaust Weight (g / mole)
20.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.09
| RFNA-Ammonia ${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 2.18 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,487 Reference Velocity (exhaust m / s) 1,562 Chamber Temperature (K) 2,572 Exhaust Weight (g / mole) 20.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.09 |
RFNA-Ammonia
${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Ammonia
${ NH }_{ 3 }$
Molecular Weight (Fuel)
17.030’52
Mixture Ratio (X:1)
2.18
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
278
Effective Velocity (exhaust m / s)
2,487
Reference Velocity (exhaust m / s)
1,562
Chamber Temperature (K)
2,572
Exhaust Weight (g / mole)
20.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.09
| RFNA-Ammonia ${ HNO }_{ 3 }$ ⋅ ${ NH }_{ 3 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Ammonia ${ NH }_{ 3 }$ Molecular Weight (Fuel) 17.030’52 Mixture Ratio (X:1) 2.18 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 278 Effective Velocity (exhaust m / s) 2,487 Reference Velocity (exhaust m / s) 1,562 Chamber Temperature (K) 2,572 Exhaust Weight (g / mole) 20.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.09 |
RFNA-Aniline
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
3.31
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,451
Reference Velocity (exhaust m / s)
1,539
Chamber Temperature (K)
3,160
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.36
| RFNA-Aniline ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 3.31 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,451 Reference Velocity (exhaust m / s) 1,539 Chamber Temperature (K) 3,160 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.36 |
RFNA-Aniline
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
3.31
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,451
Reference Velocity (exhaust m / s)
1,539
Chamber Temperature (K)
3,160
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.36
| RFNA-Aniline ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 3.31 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,451 Reference Velocity (exhaust m / s) 1,539 Chamber Temperature (K) 3,160 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.36 |
RFNA-Aniline
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
3.31
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,451
Reference Velocity (exhaust m / s)
1,539
Chamber Temperature (K)
3,160
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.36
| RFNA-Aniline ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 3.31 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,451 Reference Velocity (exhaust m / s) 1,539 Chamber Temperature (K) 3,160 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.36 |
RFNA-Aniline
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
3.31
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,451
Reference Velocity (exhaust m / s)
1,539
Chamber Temperature (K)
3,160
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.36
| RFNA-Aniline ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 3.31 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,451 Reference Velocity (exhaust m / s) 1,539 Chamber Temperature (K) 3,160 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.36 |
RFNA-Aniline
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Aniline
${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$
Molecular Weight (Fuel)
93.126’48
Mixture Ratio (X:1)
3.31
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,451
Reference Velocity (exhaust m / s)
1,539
Chamber Temperature (K)
3,160
Exhaust Weight (g / mole)
26.20
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.36
| RFNA-Aniline ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Aniline ${ C }_{ 6 }{ H }_{ 5 }{ NH }_{ 2 }$ Molecular Weight (Fuel) 93.126’48 Mixture Ratio (X:1) 3.31 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,451 Reference Velocity (exhaust m / s) 1,539 Chamber Temperature (K) 3,160 Exhaust Weight (g / mole) 26.20 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.36 |
RFNA-Ethanol-75
${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.30
Specific Impulse (seconds @ sl)
244
Density Impulse (kg · s · l @ sl)
296
Effective Velocity (exhaust m / s)
2,391
Reference Velocity (exhaust m / s)
1,492
Chamber Temperature (K)
2,758
Exhaust Weight (g / mole)
24.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.21
| RFNA-Ethanol-75 ${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.30 Specific Impulse (seconds @ sl) 244 Density Impulse (kg · s · l @ sl) 296 Effective Velocity (exhaust m / s) 2,391 Reference Velocity (exhaust m / s) 1,492 Chamber Temperature (K) 2,758 Exhaust Weight (g / mole) 24.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.21 |
RFNA-Ethanol-75
${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.30
Specific Impulse (seconds @ sl)
244
Density Impulse (kg · s · l @ sl)
296
Effective Velocity (exhaust m / s)
2,391
Reference Velocity (exhaust m / s)
1,492
Chamber Temperature (K)
2,758
Exhaust Weight (g / mole)
24.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.21
| RFNA-Ethanol-75 ${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.30 Specific Impulse (seconds @ sl) 244 Density Impulse (kg · s · l @ sl) 296 Effective Velocity (exhaust m / s) 2,391 Reference Velocity (exhaust m / s) 1,492 Chamber Temperature (K) 2,758 Exhaust Weight (g / mole) 24.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.21 |
RFNA-Ethanol-75
${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.30
Specific Impulse (seconds @ sl)
244
Density Impulse (kg · s · l @ sl)
296
Effective Velocity (exhaust m / s)
2,391
Reference Velocity (exhaust m / s)
1,492
Chamber Temperature (K)
2,758
Exhaust Weight (g / mole)
24.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.21
| RFNA-Ethanol-75 ${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.30 Specific Impulse (seconds @ sl) 244 Density Impulse (kg · s · l @ sl) 296 Effective Velocity (exhaust m / s) 2,391 Reference Velocity (exhaust m / s) 1,492 Chamber Temperature (K) 2,758 Exhaust Weight (g / mole) 24.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.21 |
RFNA-Ethanol-75
${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.30
Specific Impulse (seconds @ sl)
244
Density Impulse (kg · s · l @ sl)
296
Effective Velocity (exhaust m / s)
2,391
Reference Velocity (exhaust m / s)
1,492
Chamber Temperature (K)
2,758
Exhaust Weight (g / mole)
24.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.21
| RFNA-Ethanol-75 ${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.30 Specific Impulse (seconds @ sl) 244 Density Impulse (kg · s · l @ sl) 296 Effective Velocity (exhaust m / s) 2,391 Reference Velocity (exhaust m / s) 1,492 Chamber Temperature (K) 2,758 Exhaust Weight (g / mole) 24.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.21 |
RFNA-Ethanol-75
${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.30
Specific Impulse (seconds @ sl)
244
Density Impulse (kg · s · l @ sl)
296
Effective Velocity (exhaust m / s)
2,391
Reference Velocity (exhaust m / s)
1,492
Chamber Temperature (K)
2,758
Exhaust Weight (g / mole)
24.70
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.21
| RFNA-Ethanol-75 ${ HNO }_{ 3 }$ ⋅ 75% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 25% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.30 Specific Impulse (seconds @ sl) 244 Density Impulse (kg · s · l @ sl) 296 Effective Velocity (exhaust m / s) 2,391 Reference Velocity (exhaust m / s) 1,492 Chamber Temperature (K) 2,758 Exhaust Weight (g / mole) 24.70 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.21 |
RFNA-Ethanol-95
${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.75
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
305
Effective Velocity (exhaust m / s)
2,449
Reference Velocity (exhaust m / s)
1,530
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.22
| RFNA-Ethanol-95 ${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.75 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 305 Effective Velocity (exhaust m / s) 2,449 Reference Velocity (exhaust m / s) 1,530 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.22 |
RFNA-Ethanol-95
${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.75
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
305
Effective Velocity (exhaust m / s)
2,449
Reference Velocity (exhaust m / s)
1,530
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.22
| RFNA-Ethanol-95 ${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.75 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 305 Effective Velocity (exhaust m / s) 2,449 Reference Velocity (exhaust m / s) 1,530 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.22 |
RFNA-Ethanol-95
${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.75
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
305
Effective Velocity (exhaust m / s)
2,449
Reference Velocity (exhaust m / s)
1,530
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.22
| RFNA-Ethanol-95 ${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.75 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 305 Effective Velocity (exhaust m / s) 2,449 Reference Velocity (exhaust m / s) 1,530 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.22 |
RFNA-Ethanol-95
${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.75
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
305
Effective Velocity (exhaust m / s)
2,449
Reference Velocity (exhaust m / s)
1,530
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.22
| RFNA-Ethanol-95 ${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.75 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 305 Effective Velocity (exhaust m / s) 2,449 Reference Velocity (exhaust m / s) 1,530 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.22 |
RFNA-Ethanol-95
${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
2.75
Specific Impulse (seconds @ sl)
250
Density Impulse (kg · s · l @ sl)
305
Effective Velocity (exhaust m / s)
2,449
Reference Velocity (exhaust m / s)
1,530
Chamber Temperature (K)
2,905
Exhaust Weight (g / mole)
24.60
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.22
| RFNA-Ethanol-95 ${ HNO }_{ 3 }$ ⋅ 95% (${ C }_{ 2 }{ H }_{ 5 }{ O }$) + 5% (${ H }_{ 2 }{ O }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 2.75 Specific Impulse (seconds @ sl) 250 Density Impulse (kg · s · l @ sl) 305 Effective Velocity (exhaust m / s) 2,449 Reference Velocity (exhaust m / s) 1,530 Chamber Temperature (K) 2,905 Exhaust Weight (g / mole) 24.60 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.22 |
RFNA-HTPB
${ HNO }_{ 3 }$ ⋅ HTPB
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
4.09
Specific Impulse (seconds @ sl)
252
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,476
Reference Velocity (exhaust m / s)
1,553
Chamber Temperature (K)
3,124
Exhaust Weight (g / mole)
25.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.34
| RFNA-HTPB ${ HNO }_{ 3 }$ ⋅ HTPB Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 4.09 Specific Impulse (seconds @ sl) 252 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,476 Reference Velocity (exhaust m / s) 1,553 Chamber Temperature (K) 3,124 Exhaust Weight (g / mole) 25.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.34 |
RFNA-HTPB
${ HNO }_{ 3 }$ ⋅ HTPB
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
4.09
Specific Impulse (seconds @ sl)
252
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,476
Reference Velocity (exhaust m / s)
1,553
Chamber Temperature (K)
3,124
Exhaust Weight (g / mole)
25.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.34
| RFNA-HTPB ${ HNO }_{ 3 }$ ⋅ HTPB Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 4.09 Specific Impulse (seconds @ sl) 252 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,476 Reference Velocity (exhaust m / s) 1,553 Chamber Temperature (K) 3,124 Exhaust Weight (g / mole) 25.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.34 |
RFNA-HTPB
${ HNO }_{ 3 }$ ⋅ HTPB
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
4.09
Specific Impulse (seconds @ sl)
252
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,476
Reference Velocity (exhaust m / s)
1,553
Chamber Temperature (K)
3,124
Exhaust Weight (g / mole)
25.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.34
| RFNA-HTPB ${ HNO }_{ 3 }$ ⋅ HTPB Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 4.09 Specific Impulse (seconds @ sl) 252 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,476 Reference Velocity (exhaust m / s) 1,553 Chamber Temperature (K) 3,124 Exhaust Weight (g / mole) 25.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.34 |
RFNA-HTPB
${ HNO }_{ 3 }$ ⋅ HTPB
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
4.09
Specific Impulse (seconds @ sl)
252
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,476
Reference Velocity (exhaust m / s)
1,553
Chamber Temperature (K)
3,124
Exhaust Weight (g / mole)
25.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.34
| RFNA-HTPB ${ HNO }_{ 3 }$ ⋅ HTPB Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 4.09 Specific Impulse (seconds @ sl) 252 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,476 Reference Velocity (exhaust m / s) 1,553 Chamber Temperature (K) 3,124 Exhaust Weight (g / mole) 25.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.34 |
RFNA-HTPB
${ HNO }_{ 3 }$ ⋅ HTPB
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Solid)
Hydroxyl-Terminated Polybutadiene
HTPB
Molecular Weight (Fuel)
3,218.986’054
Mixture Ratio (X:1)
4.09
Specific Impulse (seconds @ sl)
252
Density Impulse (kg · s · l @ sl)
340
Effective Velocity (exhaust m / s)
2,476
Reference Velocity (exhaust m / s)
1,553
Chamber Temperature (K)
3,124
Exhaust Weight (g / mole)
25.50
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.34
| RFNA-HTPB ${ HNO }_{ 3 }$ ⋅ HTPB Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Solid) Hydroxyl-Terminated Polybutadiene HTPB Molecular Weight (Fuel) 3,218.986’054 Mixture Ratio (X:1) 4.09 Specific Impulse (seconds @ sl) 252 Density Impulse (kg · s · l @ sl) 340 Effective Velocity (exhaust m / s) 2,476 Reference Velocity (exhaust m / s) 1,553 Chamber Temperature (K) 3,124 Exhaust Weight (g / mole) 25.50 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.34 |
RFNA-Hydrazine
${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
341
Effective Velocity (exhaust m / s)
2,702
Reference Velocity (exhaust m / s)
1,702
Chamber Temperature (K)
2,932
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| RFNA-Hydrazine ${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 341 Effective Velocity (exhaust m / s) 2,702 Reference Velocity (exhaust m / s) 1,702 Chamber Temperature (K) 2,932 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
RFNA-Hydrazine
${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
341
Effective Velocity (exhaust m / s)
2,702
Reference Velocity (exhaust m / s)
1,702
Chamber Temperature (K)
2,932
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| RFNA-Hydrazine ${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 341 Effective Velocity (exhaust m / s) 2,702 Reference Velocity (exhaust m / s) 1,702 Chamber Temperature (K) 2,932 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
RFNA-Hydrazine
${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
341
Effective Velocity (exhaust m / s)
2,702
Reference Velocity (exhaust m / s)
1,702
Chamber Temperature (K)
2,932
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| RFNA-Hydrazine ${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 341 Effective Velocity (exhaust m / s) 2,702 Reference Velocity (exhaust m / s) 1,702 Chamber Temperature (K) 2,932 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
RFNA-Hydrazine
${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
341
Effective Velocity (exhaust m / s)
2,702
Reference Velocity (exhaust m / s)
1,702
Chamber Temperature (K)
2,932
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| RFNA-Hydrazine ${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 341 Effective Velocity (exhaust m / s) 2,702 Reference Velocity (exhaust m / s) 1,702 Chamber Temperature (K) 2,932 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
RFNA-Hydrazine
${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Tetrahydridodinitrogen
${ N }_{ 2 }{ H }_{ 4 }$
Molecular Weight (Fuel)
32.045’16
Mixture Ratio (X:1)
1.28
Specific Impulse (seconds @ sl)
276
Density Impulse (kg · s · l @ sl)
341
Effective Velocity (exhaust m / s)
2,702
Reference Velocity (exhaust m / s)
1,702
Chamber Temperature (K)
2,932
Exhaust Weight (g / mole)
19.80
Specific Heat Ratio (gamma)
1.22
Propellant Density (kg / l)
1.24
| RFNA-Hydrazine ${ HNO }_{ 3 }$ ⋅ ${ N }_{ 2 }{ H }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Tetrahydridodinitrogen ${ N }_{ 2 }{ H }_{ 4 }$ Molecular Weight (Fuel) 32.045’16 Mixture Ratio (X:1) 1.28 Specific Impulse (seconds @ sl) 276 Density Impulse (kg · s · l @ sl) 341 Effective Velocity (exhaust m / s) 2,702 Reference Velocity (exhaust m / s) 1,702 Chamber Temperature (K) 2,932 Exhaust Weight (g / mole) 19.80 Specific Heat Ratio (gamma) 1.22 Propellant Density (kg / l) 1.24 |
RFNA-Hydrogen
${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
8.00
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
147
Effective Velocity (exhaust m / s)
3,112
Reference Velocity (exhaust m / s)
1,957
Chamber Temperature (K)
2,795
Exhaust Weight (g / mole)
14.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.43
| RFNA-Hydrogen ${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 8.00 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 147 Effective Velocity (exhaust m / s) 3,112 Reference Velocity (exhaust m / s) 1,957 Chamber Temperature (K) 2,795 Exhaust Weight (g / mole) 14.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.43 |
RFNA-Hydrogen
${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
8.00
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
147
Effective Velocity (exhaust m / s)
3,112
Reference Velocity (exhaust m / s)
1,957
Chamber Temperature (K)
2,795
Exhaust Weight (g / mole)
14.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.43
| RFNA-Hydrogen ${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 8.00 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 147 Effective Velocity (exhaust m / s) 3,112 Reference Velocity (exhaust m / s) 1,957 Chamber Temperature (K) 2,795 Exhaust Weight (g / mole) 14.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.43 |
RFNA-Hydrogen
${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
8.00
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
147
Effective Velocity (exhaust m / s)
3,112
Reference Velocity (exhaust m / s)
1,957
Chamber Temperature (K)
2,795
Exhaust Weight (g / mole)
14.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.43
| RFNA-Hydrogen ${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 8.00 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 147 Effective Velocity (exhaust m / s) 3,112 Reference Velocity (exhaust m / s) 1,957 Chamber Temperature (K) 2,795 Exhaust Weight (g / mole) 14.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.43 |
RFNA-Hydrogen
${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
8.00
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
147
Effective Velocity (exhaust m / s)
3,112
Reference Velocity (exhaust m / s)
1,957
Chamber Temperature (K)
2,795
Exhaust Weight (g / mole)
14.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.43
| RFNA-Hydrogen ${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 8.00 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 147 Effective Velocity (exhaust m / s) 3,112 Reference Velocity (exhaust m / s) 1,957 Chamber Temperature (K) 2,795 Exhaust Weight (g / mole) 14.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.43 |
RFNA-Hydrogen
${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Hydrogen
${ H }_{ 2 }$
Molecular Weight (Fuel)
2.015’88
Mixture Ratio (X:1)
8.00
Specific Impulse (seconds @ sl)
317
Density Impulse (kg · s · l @ sl)
147
Effective Velocity (exhaust m / s)
3,112
Reference Velocity (exhaust m / s)
1,957
Chamber Temperature (K)
2,795
Exhaust Weight (g / mole)
14.30
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
0.43
| RFNA-Hydrogen ${ HNO }_{ 3 }$ ⋅ ${ H }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Hydrogen ${ H }_{ 2 }$ Molecular Weight (Fuel) 2.015’88 Mixture Ratio (X:1) 8.00 Specific Impulse (seconds @ sl) 317 Density Impulse (kg · s · l @ sl) 147 Effective Velocity (exhaust m / s) 3,112 Reference Velocity (exhaust m / s) 1,957 Chamber Temperature (K) 2,795 Exhaust Weight (g / mole) 14.30 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 0.43 |
RFNA-Kerosene
${ HNO }_{ 3 }$ ⋅ RP-1
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
4.42
Specific Impulse (seconds @ sl)
256
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,514
Reference Velocity (exhaust m / s)
1,576
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
24.40
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.31
| RFNA-Kerosene ${ HNO }_{ 3 }$ ⋅ RP-1 Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 4.42 Specific Impulse (seconds @ sl) 256 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,514 Reference Velocity (exhaust m / s) 1,576 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 24.40 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.31 |
RFNA-Kerosene
${ HNO }_{ 3 }$ ⋅ RP-1
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
4.42
Specific Impulse (seconds @ sl)
256
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,514
Reference Velocity (exhaust m / s)
1,576
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
24.40
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.31
| RFNA-Kerosene ${ HNO }_{ 3 }$ ⋅ RP-1 Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 4.42 Specific Impulse (seconds @ sl) 256 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,514 Reference Velocity (exhaust m / s) 1,576 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 24.40 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.31 |
RFNA-Kerosene
${ HNO }_{ 3 }$ ⋅ RP-1
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
4.42
Specific Impulse (seconds @ sl)
256
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,514
Reference Velocity (exhaust m / s)
1,576
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
24.40
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.31
| RFNA-Kerosene ${ HNO }_{ 3 }$ ⋅ RP-1 Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 4.42 Specific Impulse (seconds @ sl) 256 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,514 Reference Velocity (exhaust m / s) 1,576 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 24.40 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.31 |
RFNA-Kerosene
${ HNO }_{ 3 }$ ⋅ RP-1
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
4.42
Specific Impulse (seconds @ sl)
256
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,514
Reference Velocity (exhaust m / s)
1,576
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
24.40
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.31
| RFNA-Kerosene ${ HNO }_{ 3 }$ ⋅ RP-1 Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 4.42 Specific Impulse (seconds @ sl) 256 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,514 Reference Velocity (exhaust m / s) 1,576 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 24.40 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.31 |
RFNA-Kerosene
${ HNO }_{ 3 }$ ⋅ RP-1
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Kerosene
RP-1
Molecular Weight (Fuel)
13.976’183
Mixture Ratio (X:1)
4.42
Specific Impulse (seconds @ sl)
256
Density Impulse (kg · s · l @ sl)
335
Effective Velocity (exhaust m / s)
2,514
Reference Velocity (exhaust m / s)
1,576
Chamber Temperature (K)
3,076
Exhaust Weight (g / mole)
24.40
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.31
| RFNA-Kerosene ${ HNO }_{ 3 }$ ⋅ RP-1 Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Kerosene RP-1 Molecular Weight (Fuel) 13.976’183 Mixture Ratio (X:1) 4.42 Specific Impulse (seconds @ sl) 256 Density Impulse (kg · s · l @ sl) 335 Effective Velocity (exhaust m / s) 2,514 Reference Velocity (exhaust m / s) 1,576 Chamber Temperature (K) 3,076 Exhaust Weight (g / mole) 24.40 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.31 |
RFNA-Methane
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
5.32
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
281
Effective Velocity (exhaust m / s)
2,561
Reference Velocity (exhaust m / s)
1,603
Chamber Temperature (K)
2,971
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.08
| RFNA-Methane ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 5.32 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 281 Effective Velocity (exhaust m / s) 2,561 Reference Velocity (exhaust m / s) 1,603 Chamber Temperature (K) 2,971 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.08 |
RFNA-Methane
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
5.32
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
281
Effective Velocity (exhaust m / s)
2,561
Reference Velocity (exhaust m / s)
1,603
Chamber Temperature (K)
2,971
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.08
| RFNA-Methane ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 5.32 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 281 Effective Velocity (exhaust m / s) 2,561 Reference Velocity (exhaust m / s) 1,603 Chamber Temperature (K) 2,971 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.08 |
RFNA-Methane
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
5.32
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
281
Effective Velocity (exhaust m / s)
2,561
Reference Velocity (exhaust m / s)
1,603
Chamber Temperature (K)
2,971
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.08
| RFNA-Methane ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 5.32 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 281 Effective Velocity (exhaust m / s) 2,561 Reference Velocity (exhaust m / s) 1,603 Chamber Temperature (K) 2,971 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.08 |
RFNA-Methane
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
5.32
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
281
Effective Velocity (exhaust m / s)
2,561
Reference Velocity (exhaust m / s)
1,603
Chamber Temperature (K)
2,971
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.08
| RFNA-Methane ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 5.32 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 281 Effective Velocity (exhaust m / s) 2,561 Reference Velocity (exhaust m / s) 1,603 Chamber Temperature (K) 2,971 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.08 |
RFNA-Methane
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methane
${ CH }_{ 4 }$
Molecular Weight (Fuel)
16.042’46
Mixture Ratio (X:1)
5.32
Specific Impulse (seconds @ sl)
261
Density Impulse (kg · s · l @ sl)
281
Effective Velocity (exhaust m / s)
2,561
Reference Velocity (exhaust m / s)
1,603
Chamber Temperature (K)
2,971
Exhaust Weight (g / mole)
22.90
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.08
| RFNA-Methane ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 4 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methane ${ CH }_{ 4 }$ Molecular Weight (Fuel) 16.042’46 Mixture Ratio (X:1) 5.32 Specific Impulse (seconds @ sl) 261 Density Impulse (kg · s · l @ sl) 281 Effective Velocity (exhaust m / s) 2,561 Reference Velocity (exhaust m / s) 1,603 Chamber Temperature (K) 2,971 Exhaust Weight (g / mole) 22.90 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.08 |
RFNA-Methanol
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,441
Reference Velocity (exhaust m / s)
1,524
Chamber Temperature (K)
2,824
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.17
| RFNA-Methanol ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,441 Reference Velocity (exhaust m / s) 1,524 Chamber Temperature (K) 2,824 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.17 |
RFNA-Methanol
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,441
Reference Velocity (exhaust m / s)
1,524
Chamber Temperature (K)
2,824
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.17
| RFNA-Methanol ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,441 Reference Velocity (exhaust m / s) 1,524 Chamber Temperature (K) 2,824 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.17 |
RFNA-Methanol
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,441
Reference Velocity (exhaust m / s)
1,524
Chamber Temperature (K)
2,824
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.17
| RFNA-Methanol ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,441 Reference Velocity (exhaust m / s) 1,524 Chamber Temperature (K) 2,824 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.17 |
RFNA-Methanol
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,441
Reference Velocity (exhaust m / s)
1,524
Chamber Temperature (K)
2,824
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.17
| RFNA-Methanol ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,441 Reference Velocity (exhaust m / s) 1,524 Chamber Temperature (K) 2,824 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.17 |
RFNA-Methanol
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Methyl Alcohol
${ CH }_{ 3 }{ OH }$
Molecular Weight (Fuel)
32.041’86
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
249
Density Impulse (kg · s · l @ sl)
292
Effective Velocity (exhaust m / s)
2,441
Reference Velocity (exhaust m / s)
1,524
Chamber Temperature (K)
2,824
Exhaust Weight (g / mole)
24.20
Specific Heat Ratio (gamma)
1.19
Propellant Density (kg / l)
1.17
| RFNA-Methanol ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 3 }{ OH }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Methyl Alcohol ${ CH }_{ 3 }{ OH }$ Molecular Weight (Fuel) 32.041’86 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 249 Density Impulse (kg · s · l @ sl) 292 Effective Velocity (exhaust m / s) 2,441 Reference Velocity (exhaust m / s) 1,524 Chamber Temperature (K) 2,824 Exhaust Weight (g / mole) 24.20 Specific Heat Ratio (gamma) 1.19 Propellant Density (kg / l) 1.17 |
RFNA-MMH
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,658
Chamber Temperature (K)
3,033
Exhaust Weight (g / mole)
21.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-MMH ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,658 Chamber Temperature (K) 3,033 Exhaust Weight (g / mole) 21.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-MMH
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,658
Chamber Temperature (K)
3,033
Exhaust Weight (g / mole)
21.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-MMH ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,658 Chamber Temperature (K) 3,033 Exhaust Weight (g / mole) 21.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-MMH
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,658
Chamber Temperature (K)
3,033
Exhaust Weight (g / mole)
21.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-MMH ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,658 Chamber Temperature (K) 3,033 Exhaust Weight (g / mole) 21.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-MMH
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,658
Chamber Temperature (K)
3,033
Exhaust Weight (g / mole)
21.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-MMH ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,658 Chamber Temperature (K) 3,033 Exhaust Weight (g / mole) 21.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-MMH
${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Monomethylhydrazine
${ CH }_{ 6 }{ N }_{ 2 }$
Molecular Weight (Fuel)
46.071’74
Mixture Ratio (X:1)
2.13
Specific Impulse (seconds @ sl)
269
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,635
Reference Velocity (exhaust m / s)
1,658
Chamber Temperature (K)
3,033
Exhaust Weight (g / mole)
21.70
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.22
| RFNA-MMH ${ HNO }_{ 3 }$ ⋅ ${ CH }_{ 6 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Monomethylhydrazine ${ CH }_{ 6 }{ N }_{ 2 }$ Molecular Weight (Fuel) 46.071’74 Mixture Ratio (X:1) 2.13 Specific Impulse (seconds @ sl) 269 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,635 Reference Velocity (exhaust m / s) 1,658 Chamber Temperature (K) 3,033 Exhaust Weight (g / mole) 21.70 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.22 |
RFNA-Tonka-250
${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.79
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,488
Reference Velocity (exhaust m / s)
1,560
Chamber Temperature (K)
3,087
Exhaust Weight (g / mole)
25.00
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.29
| RFNA-Tonka-250 ${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.79 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,488 Reference Velocity (exhaust m / s) 1,560 Chamber Temperature (K) 3,087 Exhaust Weight (g / mole) 25.00 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.29 |
RFNA-Tonka-250
${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.79
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,488
Reference Velocity (exhaust m / s)
1,560
Chamber Temperature (K)
3,087
Exhaust Weight (g / mole)
25.00
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.29
| RFNA-Tonka-250 ${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.79 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,488 Reference Velocity (exhaust m / s) 1,560 Chamber Temperature (K) 3,087 Exhaust Weight (g / mole) 25.00 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.29 |
RFNA-Tonka-250
${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.79
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,488
Reference Velocity (exhaust m / s)
1,560
Chamber Temperature (K)
3,087
Exhaust Weight (g / mole)
25.00
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.29
| RFNA-Tonka-250 ${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.79 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,488 Reference Velocity (exhaust m / s) 1,560 Chamber Temperature (K) 3,087 Exhaust Weight (g / mole) 25.00 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.29 |
RFNA-Tonka-250
${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.79
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,488
Reference Velocity (exhaust m / s)
1,560
Chamber Temperature (K)
3,087
Exhaust Weight (g / mole)
25.00
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.29
| RFNA-Tonka-250 ${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.79 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,488 Reference Velocity (exhaust m / s) 1,560 Chamber Temperature (K) 3,087 Exhaust Weight (g / mole) 25.00 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.29 |
RFNA-Tonka-250
${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
Fuel (Liquid)
Triethylamine (50%) Xylidine (50%)
50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$)
Molecular Weight (Fuel)
111.184’82
Mixture Ratio (X:1)
3.79
Specific Impulse (seconds @ sl)
254
Density Impulse (kg · s · l @ sl)
328
Effective Velocity (exhaust m / s)
2,488
Reference Velocity (exhaust m / s)
1,560
Chamber Temperature (K)
3,087
Exhaust Weight (g / mole)
25.00
Specific Heat Ratio (gamma)
1.20
Propellant Density (kg / l)
1.29
| RFNA-Tonka-250 ${ HNO }_{ 3 }$ ⋅ 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 Fuel (Liquid) Triethylamine (50%) Xylidine (50%) 50% (${ C }_{ 6 }{ H }_{ 15 }{ N }$) + 50% (${ C }_{ 8 }{ H }_{ 11 }{ N }$) Molecular Weight (Fuel) 111.184’82 Mixture Ratio (X:1) 3.79 Specific Impulse (seconds @ sl) 254 Density Impulse (kg · s · l @ sl) 328 Effective Velocity (exhaust m / s) 2,488 Reference Velocity (exhaust m / s) 1,560 Chamber Temperature (K) 3,087 Exhaust Weight (g / mole) 25.00 Specific Heat Ratio (gamma) 1.20 Propellant Density (kg / l) 1.29 |
RFNA-UDMH
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
266
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,605
Reference Velocity (exhaust m / s)
1,638
Chamber Temperature (K)
3,062
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-UDMH ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 266 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,605 Reference Velocity (exhaust m / s) 1,638 Chamber Temperature (K) 3,062 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-UDMH
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
266
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,605
Reference Velocity (exhaust m / s)
1,638
Chamber Temperature (K)
3,062
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-UDMH ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 266 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,605 Reference Velocity (exhaust m / s) 1,638 Chamber Temperature (K) 3,062 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-UDMH
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
266
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,605
Reference Velocity (exhaust m / s)
1,638
Chamber Temperature (K)
3,062
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-UDMH ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 266 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,605 Reference Velocity (exhaust m / s) 1,638 Chamber Temperature (K) 3,062 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-UDMH
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
266
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,605
Reference Velocity (exhaust m / s)
1,638
Chamber Temperature (K)
3,062
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-UDMH ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 266 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,605 Reference Velocity (exhaust m / s) 1,638 Chamber Temperature (K) 3,062 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |
RFNA-UDMH
${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$
Oxidiser (Liquid)
Red Fuming Nitric Acid
${ HNO }_{ 3 }$
Molecular Weight (Oxidiser)
99.990’534’9
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)
266
Density Impulse (kg · s · l @ sl)
321
Effective Velocity (exhaust m / s)
2,605
Reference Velocity (exhaust m / s)
1,638
Chamber Temperature (K)
3,062
Exhaust Weight (g / mole)
22.40
Specific Heat Ratio (gamma)
1.21
Propellant Density (kg / l)
1.21
| RFNA-UDMH ${ HNO }_{ 3 }$ ⋅ ${ C }_{ 2 }{ H }_{ 8 }{ N }_{ 2 }$ Oxidiser (Liquid) Red Fuming Nitric Acid ${ HNO }_{ 3 }$ Molecular Weight (Oxidiser) 99.990’534’9 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) 266 Density Impulse (kg · s · l @ sl) 321 Effective Velocity (exhaust m / s) 2,605 Reference Velocity (exhaust m / s) 1,638 Chamber Temperature (K) 3,062 Exhaust Weight (g / mole) 22.40 Specific Heat Ratio (gamma) 1.21 Propellant Density (kg / l) 1.21 |