Comparison of orbital rocket engines

This page is an incomplete list of orbital rocket engine data.

Engine data

This list is incomplete; you can help by expanding it.

Legend: [under development] — [operational or inactive] — [retired or canceled]

Engine Origin Designer Vehicle Use Propellant Specific impulse (s)[lower-alpha 1] Thrust (N)[lower-alpha 1] Mass (kg) Thrust/ weight ratio[lower-alpha 2] Chamber pressure (bar) Oxidiser to Fuel Ratio
Aestus  Europe Airbus Defence and Space Ariane 5 G, G+, ES Upper N2O4 / MMH 324[1] 30,000 111 27.6 11 1.9
Aestus II  Europe Airbus Defence and Space Ariane 5 Upper N2O4 / MMH 340[2] 55,400 138 41.0 60 1.9
AJ-60A  USA Aerojet Atlas V Booster Solid 275 1,270,000[3]
AR1  USA Aerojet Rocketdyne Vulcan (potential) 1st RP-1 / LOX 2,200,000 (SL)[4] 2.72
BE-3  USA Blue Origin New Glenn
New Shepard		 1st,2nd,3rd LH2 / LOX 490,000
BE-4  USA Blue Origin New Glenn
Vulcan		 1st CH4 / LOX 2,400,000[5][6] 134[7]
Boeing 601HP[lower-alpha 3]  USA Boeing Boeing 601HP satellites Ion thruster Xenon 2,568 @0.5 kW 0.018 @0.5 kW
CE-20  India LPSC GSLV Mk III Upper LH2 / LOX 443 200,000 588 60.00 5.05
CE-7.5  India LPSC GSLV Mk II Upper LH2 / LOX 454[8] 73,500 to 93,100 445 16.85 58
F-1[lower-alpha 4]  USA Rocketdyne Saturn V 1st RP-1 / LOX 304
263 (SL)		 7,770,000
6,770,000 (SL)		 8,391 82.27 70 2.27
F-1A[lower-alpha 5][9]  USA Rocketdyne 1st RP-1 / LOX 303
270 (SL)		 8,989,000
8,007,000 (SL)		 9,015 90.6 80 2.27
Gamma 2  United Kingdom Bristol Siddeley Black Arrow 2nd RP-1 / H2O2 265[10] 68,200 173 40.22 8
Gamma 8  United Kingdom Bristol Siddeley Black Arrow 1st RP-1 / H2O2 265[11] 234,800 342 70.01 47.40 8
Hadley  USA Ursa Major Technologies GOLauncher 1[12] 1st RP-1 / LOX 22,241 (SL)[13]
HiPEP[lower-alpha 6]  USA NASA Jupiter Icy Moons Orbiter Ion thruster Xenon 9,620 @39.3 kW 0.670 @39.3 kW
HM-7A  Europe Snecma Ariane 1 3rd LH2 / LOX 443[14]
308 (SL)		 61,700 149 42.2 30 5
HM-7B  Europe Snecma Ariane 2
Ariane 3
Ariane 4
Ariane 5 ECA		 Upper LH2 / LOX 446[15]
310 (SL)[16]		 64,800[15]
43,600 (SL)[16]		 165[15] 43.25 37[15] 5
J-2  USA Rocketdyne Saturn V
Saturn IB		 2nd, 3rd LH2 / LOX 421[17]
200 (SL)		 1,033,100
486,200 (SL)		 1,438 73.18 30 5.5
J-2X  USA Pratt & Whitney Rocketdyne SLS Upper LH2 / LOX 448[18] 1,310,000 2,470 58.41 95 5.5-4.5
LE-5  Japan Mitsubishi
NASDA		 H-I Upper LH2 / LOX 450[19] 103,000 245 42.87 36.0 5.5
LE-5A  Japan Mitsubishi
NASDA		 H-II Upper LH2 / LOX 452[20] 121,500 242 51.19 40.0 5
LE-5B  Japan Mitsubishi
JAXA		 H-IIA
H-IIB		 Upper LH2 / LOX 447[21] 137,000 269 51.93 36.0 5
LE-7  Japan Mitsubishi
NASDA		 H-II 1st LH2 / LOX 446[22] 1,078,000
843,500 (SL)		 1,714 64.13 127 5.9
LE-7A  Japan Mitsubishi
JAXA		 H-IIA
H-IIB		 1st LH2 / LOX 438[23]
338 (SL)[23]		 1,098,000 1,800 62.2 121 5.9
Lightning 1[24]  USA Firefly Aerospace Alpha 2nd RP-1 / LOX 322 70,100
Merlin 1C  USA SpaceX
1st,2nd RP-1 / LOX 304[25]
266 (SL)[26]		 480,408[25]
422,581 (SL)[25]		 630 92[25] 67.7
Merlin 1D  USA SpaceX Falcon 9 v1.1 1st RP-1 / LOX 311[27]
282 (SL)[27]		 723,000[28] 470[28] 158[28] 97 2.34
Merlin 1D FT  USA SpaceX Falcon 9 FT
Falcon Heavy		 1st RP-1 / LOX 311[27]
282 (SL)[27]		 914,000[29]
845,000 (SL)[29]		 470[28] 199.5[29]
Merlin Vacuum 1C  USA SpaceX
2nd RP-1 / LOX 336[26] 413,644[26] 92
Merlin Vacuum 1D  USA SpaceX Falcon 9
Falcon Heavy		 2nd RP-1 / LOX 348[30] 934,000[30] 2.36
Mira (LM10)  Italy Avio Vega E[31] 3rd[31] CH4/LOX[31] 362.3 [31] 98,100 [31] 250 [31] 40 [31] 3.4 [31]
NewtonThree  USA Virgin Galactic LauncherOne Booster RP-1 / LOX 266,893[32]
NewtonFour  USA Virgin Galactic LauncherOne 2nd RP-1 / LOX 22,241[32]
NEXT  USA NASA Ion thruster Xenon 4,100 @6.9 kW 0.236 @6.9 kW
NK-33A (AJ26-62)
11Д111 / 14Д15		  Soviet Union JSC Kuznetsov Antares 100
Soyuz-2-1v		 1st RP-1 / LOX 331[33] 1,638,000 1,222 136.8 145
NSTAR[34][35][lower-alpha 7]  USA Hughes Electron Dynamics
Boeing		 Deep Space 1
Dawn		 Ion thruster Xenon 3,100 @2.3 kW 0.0920 @2.3 kW 8.2
P80[36][37]:5[38]  Europe Vega 1st HTPB 280 2,261,000 96,000 with fuel
P120C[39]  Europe Ariane 6/Vega-C Booster/1st HTPB[40] 279[39] 4,650,000[39] 161,000 with fuel[39]
P230  Europe SNPE and Avio Spa (Italy) Ariane 5 Booster HTPB 286[41]
259 (SL)		 6,470,000
5,860,000 (SL)		 269,000 with fuel[41]
PPS-1350 (СПД-100)  Russia
 OKB Fakel SMART-1 Hall thruster Xenon 1,650 @1.5 kW 0.088 @1.5 kW 5.3
S139  India SDSC PSLV 1st HTPB 269[42] 4,860,000 160,200
with fuel		 58
Raptor[43]  USA SpaceX BFR 1st, 2nd CH4 / LOX 356[44]
330 (SL)		 1,700,000 (SL) 300[45] 3.8
Raptor Vacuum[43]  USA SpaceX BFR 2nd, 1st on Mars CH4 / LOX 380+[46] 1,900,000[44] 300[45] 3.8
RD-0120
11Д122		  Soviet Union KBKhA Energia 1st LH2 / LOX 455[47] 1,962,000 3,450 57.80 219
RD-0124
14Д23		  Russia KBKhA Soyuz-2.1b
Soyuz-2-1v
Angara		 2nd, 3rd RP-1 / LOX 359[48] 294,300 520 57.7 160
RD-107A
14Д22		  Russia NPO Energomash Soyuz-FG
Soyuz-2		 1st RP-1 / LOX 320.2[49]
263.3 (SL)		 1,019,892
839,449 (SL)		 1,090 78.53 61.2
RD-108A
14Д21		  Russia NPO Energomash Soyuz-FG
Soyuz-2		 2nd RP-1 / LOX 320.6[49]
257.7 (SL)		 921,825
792,377 (SL)		 1,075 75.16 55.5
RD-117
11Д511		  Soviet Union NPO Energomash Soyuz-U 1st RP-1 / LOX 316[50]
253 (SL)		 978,000
778,648 (SL)		 1,100 72.18 54.2
RD-118
11Д512		  Soviet Union NPO Energomash Soyuz-U 2nd RP-1 / LOX 314[50]
257 (SL)		 1,000,278
818,855 (SL)		 1,100 75.91 59.7
RD-171M[lower-alpha 8]11Д520  Russia NPO Energomash Zenit-2M
Zenit-3SL
Zenit-3SLB
Zenit-3SLBF		 1st RP-1 / LOX 337.2[51]
309.5 (SL)		 7,904,160
7,256,921 (SL)		 9,300 79.57 250
RD-170[lower-alpha 8]11Д521  Soviet Union NPO Energomash Energia 1st RP-1 / LOX 337.2
309.5 (SL)		 7,904,160
7,256,921 (SL)		 9,300 79.57 250
RD-180  Russia NPO Energomash Atlas V
Atlas III		 1st RP-1 / LOX 338.4[52]
311.9 (SL)		 4,152,136
3,826,555 (SL)		 5,480 71.2 261.7 2.72
RD-181  Russia NPO Energomash Antares 200 1st RP-1 / LOX 339.2[53]
311.9 (SL)		 2,085,000
1,922,000 (SL)		 2,200 89 262.6
RD-191  Russia NPO Energomash Angara 1st RP-1 / LOX 337.5[54]
311.2 (SL)		 2,084,894
1,922,103 (SL)		 2,200 89.09 262.6
RD-193  Russia NPO Energomash Soyuz-2-1v 1st RP-1 / LOX 337.5[55]
311.2		 2,084,894
1,922,103 (SL)		 1,900 103.15
RD-264
11Д119		  Soviet Union NPO Energomash Dnepr 1st N2O4 / UDMH 318[56]
293 (SL)		 4,521,000 3,600 128.15 206
RD-275M
14Д14М		  Russia NPO Energomash Proton-M 1st N2O4 / UDMH 315.8[57]
288 (SL)		 1,831,882
1,671,053 (SL)		 1,070 159.25 165.2
RD-56 (KVD-1)
11Д56У		  Russia KBKhM GSLV Mk I Upper LH2 / LOX 462[58] 69,626 282 25.17 55.9
Reaver 1[24]  USA Firefly Aerospace Alpha 1st RP-1 / LOX 295.6 184,000
RL-10A-4-2[59]  USA Aerojet Rocketdyne Atlas IIIB
Atlas V		 Upper LH2 / LOX 451 99,100 167 60.5 39
RL-10B-2[60]  USA Aerojet Rocketdyne Delta III
Delta IV
SLS		 Upper LH2 / LOX 462 109,890 277 40.5 44
RL-10C-1[61]  USA Aerojet Rocketdyne Delta III
Delta IV
SLS,
Vulcan		 Upper LH2 / LOX 470 110,000 277 40.5 44
RS-25 (SSME)[lower-alpha 9]  USA Rocketdyne Space Shuttle
SLS		 1st LH2 / LOX 452.3 2,279,000
1,860,000 (SL)[62]		 3,526 53.79 206.4
RS-68A[lower-alpha 10]  USA Rocketdyne Delta IV
Delta IV Heavy		 1st LH2 / LOX 414[63] 3,560,000
3,137,000 (SL)		 6,747 53.80 196
Rutherford  New Zealand Rocket Lab Electron 1st, 2nd RP-1 / LOX 327 22,000
16,890 (SL)
S200  India SDSC GSLV Mk III Booster HTPB 274.5[64] 5,150,000[65][66][67] 207,000
with fuel[64]
SCE-200  India LPSC GSLV Mk III
ULV		 Upper / Main RP-1 / LOX 335
299 (SL)		 2,030,000
1,820,000 (SL)		 2,700 180
SLS Solid Rocket Booster[lower-alpha 11]  USA Orbital ATK SLS Booster PBAN 267 16,000,000 730,000
with fuel
SLV-1  India Godrej & Boyce PSLV Booster HTPB 253[68] 502,600 10,800
with fuel		 43
Space Shuttle Solid Rocket Booster[lower-alpha 12]  USA Thiokol Space Shuttle
Ares I		 Booster PBAN / APCP 268 14,000,000
12,500,000 (SL)		 590,000
with fuel
SPT-100  Russia OKB Fakel LS-1300 satellites Hall thruster Xenon 1,500 @1.35 kW 0.083 @1.35 kW 3.5
SRB-A  Japan IHI Aerospace
JAXA		 H-IIA Booster HTPB 280[69] 2,250,000 76,400 with fuel 118
SRB-A3  Japan IHI Aerospace
JAXA		 H-IIB
Epsilon		 Booster BP-207J[70] 283.6[70] 2,305,000
2,150,000 (SL)		 76,600
with fuel		 111
UA1207  USA United Technologies Titan IV Booster PBAN 272[71]
245 (SL)		 7,116,000
6,410,400 (SL)		 319,330
with fuel
VASIMR  USA Ad Astra Rocket Company Electro-magnetic thruster Argon 5,000 @200 kW 5.7 @200 kW
Vikas (rocket engine)  India LPSC
Second / Main / Booster N2O4 / UDMH 262 680,500–804,500 V
600,500–756,500 (SL)		 53.0–58.5
Viking 2  Europe Snecma Ariane 1 1st N2O4 / UDMH 690,000
611,200 (SL)		 776 90.67
Viking 2B  Europe Snecma Ariane 2
Ariane 3		 1st N2O4 / UH 25 643,000 (SL) 776 84.5
Viking 4  Europe Snecma Ariane 1 2nd N2O4 / UDMH 713,000 826 88
Viking 4B  Europe Snecma Ariane 2
Ariane 3
Ariane 4		 2nd N2O4 / UH 25 800,000 826 98.76
Viking 5C  Europe Snecma Ariane 4 1st N2O4 / UH 25 758,000
678,000 (SL)		 826 93.57
Viking 6  Europe Snecma Ariane 4 Booster N2O4 / UH 25 750,000 826 92.59
Vinci  Europe Snecma Ariane 6 Upper LH2 / LOX 467[72] 180,000 280 65.60 61
Vulcain
HM-60		  Europe Snecma Ariane 5 1st LH2 / LOX 439[73]
326 (SL)[74]		 1,113,000[73]
773,200 (SL)[74]		 1,300[74] 84.38 109[73]
Vulcain 2  Europe Snecma Ariane 5 1st LH2 / LOX 429[75]
318 (SL)[76]		 1,359,000[75]
939,500 (SL)[76]		 1,800[74] 77.04 117.3[75]
Waxwing  United Kingdom Bristol Aerojet Black Arrow Upper Solid 278[77]
245 (SL)		 29,400
25,900 (SL)		 87 34.48
XIPS-25  USA Boeing Boeing 702 satellites Ion thruster Xenon 3,500 @4.5 kW 0.165 @4.5 kW
YF-100  China AALPT
Boosters, 1st RP-1 / LOX 335[78]
300 (SL)		 1,340,000
1,200,000 (SL)		 180
YF-115  China AALPT
2nd RP-1 / LOX 341.5 176,500
YF-21B  China AALPT
Boosters, 1st N2O4 / UDMH 260.66 (SL)[79] 2,961,600 (SL)[79]
YF-21C  China AALPT
1st N2O4 / UDMH 260.7 (SL)[79] 2,961,600 (SL)[79]
YF-25  China AALPT
Boosters N2O4 / UDMH 260.66 (SL)[79] 740,400 (SL)[79]
YF-22B  China AALPT
2nd N2O4 / UDMH 298.0[79] 738,400
YF-22C  China AALPT
2nd N2O4 / UDMH 298.0[79] 742,040
YF-22D  China AALPT
2nd N2O4 / UDMH 298.0[79] 741,400
YF-22E  China AALPT
2nd N2O4 / UDMH 298.0[79] 741,400
YF-40  China AALPT
3rd N2O4 / UDMH 303 103,000
YF-50D  China AALPT
Upper N2O4 / UDMH 315.5 6,500
YF-73  China AALPT Long March 3 3rd LH2 / LOX 420.0 44,150
YF-75  China AALPT
3rd LH2 / LOX 438.0[79] 167,170
YF-75D  China AALPT Long March 5 2nd LH2 / LOX 442.0 86,260
YF-77  China AALPT Long March 5 1st LH2 / LOX 430

310.2 (SL)

 700,000

510,000 (SL)

 2,700 102
Rodong-1  North Korea Korean Committee of Space Technology Paektusan/Unha[80][81] 1st UDMH/AK27 95/120 280,000/1,200,000

See also

Notes

  1. 1 2 Default for vacuum, SL for sea level
  2. ↑ Computed as
  3. ↑ First ever ion engine used as a main engine on an operational commercial satellite (PAS-5)
  4. ↑ Most powerful single-chamber liquid-fueled rocket engine ever developed
  5. ↑ Tested but never flown
  6. ↑ Most efficient inert gas ion thruster ever built
  7. ↑ First ever ion engine used as a main engine on an operational science spacecraft (Deep Space 1)
  8. 1 2 Most powerful multi-chamber rocket engine in the world
  9. ↑ Inactive since last Shuttle flight STS-135 in 2011
  10. ↑ Most powerful hydrogen-fueled engine in the world
  11. ↑ Largest, most powerful solid-fuel rocket motor ever built
  12. ↑ Largest solid-fuel rocket motor ever flown, and the first to be used for primary propulsion on human spaceflight missions

References

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  3. ↑ "Atlas V Solid Rocket Motor". Aerojet Rocketdyne. Retrieved 2015-06-02.
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  6. ↑ "BE-4". Blue Origin. Archived from the original on 17 September 2014. Retrieved 17 September 2014.
  7. ↑ Berger, Eric (2016-03-09). "Behind the curtain: Ars goes inside Blue Origin's secretive rocket factory". Ars Technica. Retrieved 2016-03-09.
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  9. ↑ Alternate Propulsion Subsystem Concepts NAS8-39210 DCN 1-1-PP-02147
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  81. ↑ http://www.b14643.de/Spacerockets_1/Rest_World/Paektusan-1/Description/Frame.htm
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