| |
Model 39
Propellant:   
Chamber pressure: 15 atm
Thrust: 31,000 kgf (v)
Thrust: 27,227 kgf (sl)
Burn time: 65 s
Specific impulse: 237 s (v)
Specific impulse: 203 s (sl)
Vehicles: A4, Bumper
First flight: 1946 |
|
A6 (NAA 75-110)
Propellant:
Thrust: 42,246 kgf (v)
Thrust: 37,468 kgf (sl)
Burn time: 155 s
Specific impulse: 265 s (v)
Specific impulse: 235 s (sl)
Vehicles: Redstone (1 st.)
First flight: 1953 |
|
A7 (NAA 75-110)
Thrust: 42,440 kgf (v)
Thrust: 37,635 kgf (sl)
Burn time: 155 s
Specific impulse: 265 s (v)
Specific impulse: 235 s (sl)
Vehicles: Jupiter C, Juno (1 st.)
First flight: 1956 |
|
Wasserfall engine
Propellant:  
Thrust: 9,013 kgf (v)
Thrust: 8,001 kgf (sl)
Burn time: 40 s |
Propellant: 
Vehicles: Hermes A1 / A3 |
|
|
XLR-10
Propellant:
Thrust: 9,432 kgf (v)
Thrust: 11,267 kgf (sl)
Burn time: 145 s
Specific impulse: 214 s (v)
Specific impulse: 179 s (sl)
Vehicles: Viking
First flight: 1949 |
|
|
X-405
Propellant:
Chamber pressure: 41 atm
Thrust: 13,745 kgf (v)
Thrust: 12,625 kgf (sl)
Burn time: 145 s
Specific impulse: 290 s (v)
Specific impulse: 248 s (sl)
Vehicles: Vanguard (1 st.)
First flight: 1957 |
|
LR-79-7 (MB-3-1)
Propellant: 
Chamber pressure: 40 atm
Thrust: 68,033 kgf (sl)
Burn time: 164 s
Specific impulse: 283 s (v)
Specific impulse: 250 s (sl)
Vehicles: Thor , Thor Able, Thor Burner, Thor Agena A (1 st.)
First flight: 1957 |
LR-79-7 (S-3D)
Propellant:
Vehicles: Jupiter, Juno (1 st.)
First flight:1957 |
|
LR-79-7 (MB-3-2)
Propellant:
Chamber pressure: 40 atm
Thrust: 84,819 kgf (v)
Thrust: 74.847 kgf (sl)
Specific impulse: 283 s (v)
Specific impulse: 253 s (sl)
Vehicles: Thor Able Star, Delta A / B / C (1 st.)
First flight: 1960 |
|
|
LR-79-7 (MB-3-3)
Propellant:
Chamber pressure: 40 atm
Thrust: 87,542 kgf (v)
Thrust: 77,110 kgf (sl)
Burn time: 270 s
Specific impulse: 290 s (v)
Specific impulse: 253 s (sl)
Vehicles: Thor Agena B / D, Thorad Agena D, Thor Delta,
Delta E / G / J / L / M / N / 0100 / 1000 / 2000 / 4000 (1 st.)
First flight: 1964 |
|
|
RS-27
Propellant:
Chamber pressure: 48 atm
Thrust: 104.320 kgf (v)
Thrust: 93,357 kgf (sl)
Burn time: 274 s
Specific impulse: 295 s (v)
Specific impulse: 264 s (sl)
Vehicles: Delta 3000 / 5000 (1 st.)
First flight: 1972 |
|
RS-27A
Propellant:
Chamber pressure: 48 atm
Thrust: 107.500 kgf v)
Thrust: 90,770 kgf (sl)
Burn time: 274 s
Specific impulse: 302 s (v)
Specific impulse: 255 s (sl)
Vehicles: Delta 6000 / 7000 / 7000H / 8000 (1 st.)
First flight: 1989 |
|
LR-79-7 (H-1)
Propellant:
Chamber pressure: 45 atm
Thrust: 85,275 kgf (sl)
Burn time: 150 s
Specific impulse: 289 s (v)
Specific impulse: 265 s (sl)
Vehicles: Saturn 1 / 1B (1 st.)
First flight: 1961 |
|
XLR-105-1 / 3 / 5
Vehicles: Atlas A / B / C (0, 1 st.)
First flight: 1957 / 1958 / 1958 |
LR-89-5
Propellant:
Chamber pressure: 40 atm
Thrust: 74,037 kgf (sl)
Burn time: 120 s
Specific impulse: 290 s (v)
Specific impulse: 256 s (sl) |
LR-105-5
Propellant:
Chamber pressure: 40 atm
Thrust: 27,430 kgf (sl)
Burn time: 430 s
Specific impulse: 290 s (v)
Specific impulse: 220 s (sl)
Vehicles: Atlas (0, 1 st.)
First flight: 1960 |
|
LR-89-7
Propellant:
Chamber pressure: 41 atm
Thrust: 85,162 kgf (sl)
Burn time: 174 s
Specific impulse: 294 s (v)
Specific impulse: 259 s (sl) |
LR-105-7
Propellant:
Chamber pressure: 41 atm
Thrust: 27,430 kgf (sl)
Burn time: 430 s
Specific impulse: 316 s (v)
Specific impulse: 220 s (sl)
Vehicles: Atlas (0, 1 st.)
First flight: 1963 |
|
LR-91-3
Propellant:
Chamber pressure: 41 atm
Thrust: 36,291 kgf (v)
Thrust: 24,742 kgf (sl)
Specific impulse: 308 s (v)
Vehicles: Titan 1 (2 st.)
First flight: 1959 |
|
LR-87-3
Propellant:
Chamber pressure: 39 atm
Thrust: 74,836 kgf (v)
Thrust: 66,067 kgf (sl)
Burn time: 138 s
Specific impulse: 290 s (v)
Specific impulse: 256 s (sl)
Vehicles: Titan 1 (1 st.)
First flight: 1959 |
|
|
LR-87-5
Propellant:
   
Chamber pressure: 53 atm
Thrust: 111.840 kgf (v)
Thrust: 97,534 kgf (sl)
Burn time: 155 s
Specific impulse: 297 s (v)
Specific impulse: 259 s (sl)
Vehicles: Titan 2 (1 st.)
First flight: 1962 |
|
|
LR-87-9
Propellant:
Chamber pressure: 56 atm
Thrust: 111.840 kgf (v)
Thrust: 97,534 kgf (sl)
Burn time: 155 s
Specific impulse: 297 s (v)
Specific impulse: 259 s (sl)
Vehicles: Titan 3B / C (1 st.)
First flight: 1966 |
|
LR-87-11
Propellant:
Chamber pressure: 58 atm
Thrust: 98,754 kgf (sl)
Burn time: 200 s
Specific impulse: 302 s (v)
Specific impulse: 250 s (sl)
Vehicles: Titan 3, 4 (1 st.)
First flight: 1964 |
|
LR-91-5 / 9 / 11
Propellant:
Chamber pressure: 56 atm
Thrust: 45,356-47,62 kgf (v)
Burn time: 247 s
Specific impulse: 316 s (v)
Specific impulse: 160 s (sl)
Vehicles: Titan 3, 4 (2 st.)
First flight: 1962 |
|
AJ10-37
Propellant:
Chamber pressure: 14 atm
Thrust: 3,446 kgf (v)
Specific impulse: 271 s (v)
Vehicles: Vanguard (2 st.)
First flight: 1957 |
|
|
AJ10-40 / 41 / 42
Propellant:
Chamber pressure: 14 atm
Thrust: 3,497 kgf (v)
Burn time: 115 s
Specific impulse: 270 s (v)
Vehicles: Thor Able (2 st.)
First flight: 1958 |
|
|
AJ10-101A
Propellant:
Chamber pressure: 14 atm
Thrust: 3,497 kgf (v)
Burn time: 115 s
Specific impulse: 270 s (v)
Vehicles: Thor Able (2 st.)
Vehicles: Atlas Able (3 st.)
First flight: 1958 |
|
|
AJ10-142
Propellant:
Chamber pressure: 14 atm
Thrust: 3,405 kgf (v)
Specific impulse: 270 s (v)
Vehicles: Thor -Delta (2 st.)
First flight: 1960 |
|
|
AJ10-118
Propellant:
Chamber pressure: 14 atm
Thrust: 3,446 kgf (v)
Burn time: 115 s
Specific impulse: 271 s (v)
Vehicles: Delta, Delta A (2 st.)
First flight: 1962 |
|
|
AJ10-118D
Propellant:
Chamber pressure: 14 atm
Thrust: 3,436 kg (v)
Burn time: 170 s
Specific impulse: 278 s (v)
Vehicles: Delta B / C / D (2 st.)
First flight: 1962 |
|
|
AJ10-104 / 104D
Propellant:
Chamber pressure: 14 atm
Thrust: 3,579 kgf (v)
Burn time: 278 s
Specific impulse: 296 s (v)
Vehicles: Thor Able Star (2 st.)
First flight: 1960 |
|
|
AJ10-118E
Propellant:
Chamber pressure: 14 atm
Thrust: 3,579 kgf (v)
Burn time: 400 s
Specific impulse: 278 s (v)
Vehicles: Delta E / G / J / L / M / N (2 st.)
First flight: 1965 |
|
|
AJ10-118F
Propellant:
Chamber pressure: 14 atm
Thrust: 4,221 kgf (v)
Burn time: 335 s
Specific impulse: 306 s (v)
Vehicles: Delta 0100 / 1000 (2 st.)
First flight: 1972 |
|
|
AJ10-118K
Propellant:
Chamber pressure: 9 atm
Thrust: 4,425 kgf (v)
Burn time: 444 s
Specific impulse: 321 s (v)
Vehicles: Delta 3000 / 4000 / 5000 / 6000 / 7000 / 7000H (2 st.)
First flight: 1989 |
|
|
LMDE
Propellant:
Chamber pressure: 7 atm
Thrust: 4,792 kgf (v)
Burn time: 1030 s
Specific impulse: 311 s (v)
Vehicles: Apollo LM
(descending stage)
First flight: 1968 |
|
|
TR-201
Propellant:
Chamber pressure: 7 atm
Thrust: 4,476 kgf (v)
Burn time: 322 s
Specific impulse: 303.0 s (v)
Vehicles: Delta 1000 / 2000 / 30000 (2 st.)
First flight: 1972 |
|
|
LMAE
Propellant:
Chamber pressure: 8 atm
Thrust: 1,630 kgf (v)
Burn time: 465 s
Specific impulse: 311 s (v)
Vehicles: Apollo LM
(ascending stage)
First flight: 1968 |
|
|
AJ10-137
Propellant:
Chamber pressure: 7 atm
Thrust: 9,940 kgf (v)
Burn time: 585 s
Specific impulse: 312 s (v)
Vehicles: Apollo SM
First flight: 1966 |
|
AJ10-138
Propellant:
Chamber pressure: 7 atm
Thrust: 3,630 kgf (v)
Burn time: 440 s
Specific impulse: 311 s (v)
Vehicles: Titan 3A / 3C / 3(23)C / 3(34)D / Titan 4 / 4B (Bl. Transtage)
First flight: 1964 |
|
AJ10-190 (OME)
Propellant: 
Chamber pressure: 8 atm
Thrust: 2,722 kgf (v)
Burn time: 1,250 s
Specific impulse: 316 s (v)
Vehicles: Space Shuttle (OME)
First flight: 1981 |
|
R-4D
Propellant:
Chamber pressure: 7 atm
Thrust: 50 kgf (v)
Specific impulse: 312 s (v)
Vehicles: Apollo CM
Vehicles: satellites |
|
|
R-40A
Propellant:
Thrust: 394 kgf (v)
Specific impulse: 306 s (v)
Vehicles: Space Shuttle |
|
|
Bell 8048
Propellant:
Chamber pressure: 10 atm
Thrust: 7,025 kgf (v)
Burn time: 120 s
Specific impulse: 276 s (v)
Vehicles: Thor Agena A, Atlas Agena A (2 st.)
First flight: 1959 |
|
Bell 8081
Propellant:
Chamber pressure: 10 atm
Thrust: 7,260 kgf (v)
Burn time: 240 s
Specific impulse: 285 s (v)
Vehicles: Thor Agena B, Atlas Agena B (2 st.)
First flight: 1960 |
|
Bell 8096
Propellant:
Chamber pressure: 34 atm
Thrust: 7,260 kgf
Burn time: 265 s
Specific impulse: 293 s (v)
Vehicles: Thor Agena D,
Thotrad Agena D, Atlas Agena D, Titan 3B / 3(23)B / 3(24)B / 3(33)B / 3(34)B (2 st.)
First flight: 1963 |
|
RL-10A-1
Propellant: 
Chamber pressure: 20 atm
Thrust: 6,801 kgf (v)
Burn time: 430 s
Specific impulse: 250 s (v)
Vehicles: Atlas Centaur (2 st.)
Vehicles: Saturn I (2 st.)
First flight: 1961 |
|
RL-10A-3 / 3-1 / 3-3
Propellant:
Chamber pressure: 27 atm
Thrust: 6,689 kgf (v)
Burn time: 470 s
Specific impulse: 444 s (v)
Vehicles: Atlas Centaur (2 st.)
Vehicles: Titan IIIE (3 st.)
First flight: 1967 |
|
|
RL-10A-3-3A
Propellant:
Chamber pressure: 32 atm
Thrust: 7,484 kgf (v)
Burn time: 444 s
Specific impulse: 550 s (v)
Vehicles: Atlas G / 1 / 2 (2 st.)
Vehicles:Titan 4 (3 st.)
First flight: 1984 |
|
|
RL-10A-4
Propellant:
Chamber pressure: 39-41 atm
Thrust: 9,432 kgf (v)
Burn time: 392 s
Specific impulse: 449 s (v)
Vehicles: Atlas 2A / 2As (2 st.)
First flight: 1992
|
|
RL-10A-4-1
Propellant:
Chamber pressure: 41 atm
Thrust: 9,910 kgf (v)
Burn time: 740 s
Specific impulse: 451 s (v)
Vehicles: Atlas 3 (2 st.)
First flight: 2000 |
|
|
RL-10A-4-1B
Propellant:
Chamber pressure: 41 atm
Thrust: 9,910 kgf (v)
Burn time: 740 s
Specific impulse: 451 s (v)
Vehicles: Atlas 5 (2 st.)
First flight: 2002 |
|
|
RL-10B-2
Propellant:
Chamber pressure: 44 atm
Thrust: 11,216 kgf (v)
Burn time: 700 s
Specific impulse: 462 s (v)
Vehicles: Delta 3 / 4 (2 st.)
Vehicles: SLs (2 st.)
First flight: 1998 |
|
F-1
Propellant:
Chamber pressure: 69 atm
Thrust: 822,095 kgf (v)
Thrust: 703,094 kgf (sl)
Burn time: 161 s
Specific impulse: 304 s (v)
Specific impulse: 265 s (sl)
Vehicles: Saturn V (1 st.)
First flight: 1967 |
|
J-2
Propellant:
Chamber pressure: 30 atm
Thrust: 105,350 kgf (v)
Burn time: 475 s
Specific impulse: 421 s (v)
Vehicles: Saturn 1B,
Saturn V (2, 3 st.)
First flight: 1966
|
J-2S
Propellant:
Thrust: 116,090 kgf (v)
Specific impulse: 436 s (v)
|
|
J-2X
Propellant:
Chamber pressure: 91 atm
Thrust: 133.58 kgf (v)
Burn time: 431 s
Specific impulse: 448 s (v)
Vehicles: SLs (2 st.)
|
|
RS-25 (SSME)
Propellant:
Chamber pressure: 205 atm
Thrust: 213,530 kgf (v)
Thrust: 172,940 kgf (sl)
Burn time: 480 s
Specific impulse: 453 s (v)
Specific impulse: 363 s (sl)
Vehicles: Space Shuttle (1 st.)
First flight: 1981 |
RS-25
Vehicles: SLS (1 st.)
First flight: 2022 |
|
RS-68
Propellant:
Chamber pressure: 96 atm
Thrust: 337.930 kgf (v)
Thrust: 300.730 kgf (sl)
Burn time: 249 s
Specific impulse: 420 s (v)
Specific impulse: 365 s (sl)
Vehicles: Delta IV (1 st.)
First flight: 2002 |
|
Merlin 1A
Propellant:
Chamber pressure: 53 atm
Thrust: 32,396 kgf (sl)
Burn time: 169 s
Specific impulse: 300 s (v)
Specific impulse: 169 s (sl)
Vehicles: Falcon 1 (1 st.)
First flight: 2006 |
|
|
Merlin 1Ci
Propellant:
Chamber pressure: 60 atm
Thrust: 35,557 kgf (sl)
Specific impulse: 300 s (v)
Specific impulse: 264 s (sl)
Vehicles: Falcon 1+ (1 st.)
First flight: 2008 |
|
|
Merlin 1C
Propellant:
Chamber pressure: 61 atm
Thrust: 62,681 kgf (sl)
Burn time: 169 s
Specific impulse: 304 s (v)
Specific impulse: 275 s (sl)
Vehicles: Falcon 1 / 9 v 1.0 (1 st.)
First flight: 2008 |
|
Merlin 1C+
Propellant:
Chamber pressure: 67 atm
Thrust: 62,681 kgf (sl)
Burn time: 169 s
Specific impulse: 304 s (v)
Specific impulse: 275 s (sl) |
|
|
Merlin 1D
Propellant:
Chamber pressure: 96 atm
Thrust): 73,011 kgf (sl)
Burn time: 180 s
Specific impulse: 311 s (v)
Specific impulse: 282 s (sl)
Vehicles: Falcon 9 v 1.1 (1 st.)
First flight: 2013 |
|
|
Merlin 1D+
Propellant:
Chamber pressure: 107 atm
Thrust: 77.559 kgf (sl)
Specific impulse: 320 s (v)
Specific impulse: 288 s (sl)
Vehicles: Falcon 9 v 1.2 (1 st.)
First flight: 2015 |
|
Merlin 1C-vac
Propellant:
Chamber pressure: 61 atm
Thrust: 53,524 kgf (v)
Specific impulse: 336 s (v)
Vehicles: Falcon 9 (2 st.)
First flight: 2010 |
|
|
Merlin 1D-vac
Propellant:
Chamber pressure: 96 atm
Thrust: 82,097 kgf (v)
Specific impulse: 347 s (v)
Vehicles: Falcon 9 v 1.1 (2 st.)
First flight: 2014 |
|
|
Merlin 1D+-vac
Propellant:
Chamber pressure: 107 atm
Thrust: 95,251 kgf (v)
Specific impulse: 348 s (v)
Vehicles: Falcon 9 v 1.2 (2 st.)
First flight: 2015 |
|
Raptor
Propellant: 
Chamber pressure: 266 atm
Thrust: 304.720 kgf (v)
Thrust: 170.890 kgf (sl)
Specific impulse: 355 s (v)
Specific impulse: 334 s (sl)
Vehicles: Starship, BFR (1 st.) |
|
Raptor-vac
Propellant:
Chamber pressure: 325 atm
Thrust: 317,876 kgf (v)
Thrust: 305,200 kgf (sl)
Specific impulse: 375 s (v)
Specific impulse: 360 s (sl)
Vehicles: Starship, BFR (2 st.) |
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