Analytics/Engine Dashboard
Engine Dashboard
Engines and their vehicle applications
165 engines match
Engines Tracked
165
with published thrust
Most Powerful
SLS SRB
16,000 kN vacuum
Highest ISP
NERVA
800s vacuum
Best TWR
Merlin Vacuum 1D
194 thrust-to-weight
Manufacturers
50
Most Powerful (Vacuum Thrust, kN)
Highest ISP (s, Vacuum)
All Engines
| Engine | Manufacturer | Thrust | ISP | Mass | TWR | Fuel | Used on | Source |
|---|---|---|---|---|---|---|---|---|
| SLS SRB 3D | Orbital ATK | 16,000 kN | 268s | 730,000 kg | 2.2 | PBAN | SLS Block 1 | Wikipedia |
| Space Shuttle SRB 3D | Thiokol | 14,678 kN | 268s | 590,000 kg | 2.5 | PBAN / APCP | Space Shuttle | Wikipedia |
| F-1A 3D | Rocketdyne | 8,007 kN | 304s | 8,618 kg | 95 | RP-1 / LOX | — | Wikipedia |
| RD-170 3D | NPO Energomash | 7,900 kN | 337s | 9,750 kg | 82 | RP-1 / LOX | Energiya, Energiya/Buran | Wikipedia |
| RD-171M 3D | NPO Energomash | 7,887 kN | 337s | 9,750 kg | 86 | RP-1 / LOX | Soyuz-5, Zenit-2, Zenit-3SL, Zenit-3SLB | Wikipedia |
| F-1 3D | Rocketdyne | 7,740.5 kN | 304s | 8,391 kg | 94 | RP-1 / LOX | Saturn V | Wikipedia |
| UA1207 | United Technologies | 6,948 kN | 270s | 153,800 kg | 4.6 | PBAN | Titan 34D, Titan 401B/Centaur, Titan 403B, Titan IIIC, Titan IIIE | Wikipedia |
| P230 3D | Avio | 6,470 kN | 275s | 237,000 kg | 2.8 | HTPB | Ariane 5ECA, Ariane 5ECA+, Ariane 5ES, Ariane 5ES/ATV, Ariane 5G, Ariane 5G+, Ariane 5GS | Wikipedia |
| RD-270 | NPO Energomash | 6,340 kN | 316s | 5,700 kg | 113 | UDMH / N2O4 | — | Wikipedia |
| M-1 | Aerojet | 5,340 kN | 428s | — | — | LH2 / LOX | — | Wikipedia |
| S200 3D | SDSC | 5,150 kN | 274s | 205,000 kg | 2.6 | HTPB | GSLV Mk III, LVM3 | Wikipedia |
| S139 3D | SDSC | 4,800 kN | 269s | 138,200 kg | 3.5 | HTPB | GSLV Mk I, GSLV Mk II, PSLV, PSLV-CA, PSLV-DL, PSLV-QL, PSLV-XL | Wikipedia |
| RD-264 | NPO Energomash | 4,520 kN | 318s | — | — | UDMH / N2O4 | Dnepr, Tsiklon-3 | Wikipedia |
| YF-130 | AALPT | 4,400 kN | 338s | — | — | RP-1 / LOX | — | Wikipedia |
| RD-180 3D | NPO Energomash | 4,152 kN | 339s | 5,480 kg | 77 | RP-1 / LOX | Atlas 3A, Atlas 3B, Atlas V 401, Atlas V 411, Atlas V 421, Atlas V 431, Atlas V 501, Atlas V 511, Atlas V 521, Atlas V 531, Atlas V 541, Atlas V 551, Atlas V N22 | Wikipedia |
| P120 3D | Avio | 3,650 kN | 279s | 142,000 kg | 2.6 | HTPB | Ariane 62, Ariane 64, Vega C | Wikipedia |
| RS-68A 3D | Rocketdyne | 3,370 kN | 414s | 6,597 kg | 57 | LH2 / LOX | Delta 4H, Delta 4M, Delta 4M+(4,2), Delta 4M+(5,2), Delta 4M+(5,4) | Wikipedia |
| RS-68 | Rocketdyne | 3,370 kN | 410s | 6,600 kg | 52 | LH2 / LOX | — | Wikipedia |
| P80 | Avio | 3,015 kN | 280s | 88,000 kg | 3.5 | HTPB | Vega | Wikipedia |
| YF-21C 3D | AALPT | 2,961.6 kN | 300s | — | — | UDMH / N2O4 | Chang Zheng 2D, Chang Zheng 2F, Chang Zheng 3A, Chang Zheng 3B, Chang Zheng 3C, Chang Zheng 4B, Chang Zheng 4C | Wikipedia |
| YF-21B | AALPT | 2,961.6 kN | 290s | — | — | UDMH / N2O4 | Chang Zheng 2C, Chang Zheng 3, Chang Zheng 4 | Wikipedia |
| BE-4 3D | Blue Origin | 2,800 kN | 340s | 5,400 kg | 52.8 | CH4 / LOX | New Glenn 7x2, Vulcan Centaur VC0S, Vulcan Centaur VC2S, Vulcan Centaur VC4S, Vulcan Centaur VC6S | Wikipedia |
| Raptor 3D | SpaceX | 2,747 kN | 350s | 1,525 kg | 164 | CH4 / LOX | Starship V1.0, Starship V2, Starship V3, Starship V4 | Wikipedia |
| SLV-1 | Godrej & Boyce | 2,700 kN | 269s | — | — | HTPB | — | Wikipedia |
| Raptor Vacuum 3D | SpaceX | 2,530 kN | 380s | 1,800 kg | 184 | CH4 / LOX | Starship V1.0, Starship V2, Starship V3, Starship V4 | Wikipedia |
| RS-25 3D | Rocketdyne | 2,279 kN | 452s | 3,177 kg | 73 | LH2 / LOX | SLS Block 1, Space Shuttle | Wikipedia |
| SRB-A | IHI Aerospace, JAXA | 2,255 kN | 274s | 75,900 kg | 3 | HTPB | H-II | Wikipedia |
| AR1 | Aerojet Rocketdyne | 2,200 kN | 338s | — | — | RP-1 / LOX | — | Wikipedia |
| SRB-A3 3D | IHI Aerospace, JAXA | 2,159 kN | 274s | 75,900 kg | 2.9 | HTPB | Epsilon, Epsilon-S, H-IIA 202, H-IIA 204, H-IIB, H3-22L, H3-22S, H3-24L, H3-24W | Wikipedia |
| RD-191 3D | NPO Energomash | 2,090 kN | 338s | 2,580 kg | 83 | RP-1 / LOX | Angara A5, Angara A5/Persei, Angara-1.2, Naro-1 | Wikipedia |
| RD-181 3D | NPO Energomash | 2,090 kN | 338s | 2,580 kg | 83 | RP-1 / LOX | Antares 230, Antares 230+ | Wikipedia |
| RD-193 | NPO Energomash | 2,090 kN | 338s | 2,580 kg | 83 | RP-1 / LOX | — | Wikipedia |
| RD-0120 3D | KBKhA | 1,961 kN | 455s | 3,449 kg | 62 | LH2 / LOX | Energiya, Energiya/Buran | Wikipedia |
| GEM 63XL 3D | Northrop Grumman | 1,920 kN | 274s | 30,395 kg | 6.4 | HTPB | Vulcan Centaur VC2S, Vulcan Centaur VC4S, Vulcan Centaur VC6S | Wikipedia |
| RD-253F | Energomash | 1,870 kN | 317s | — | — | UDMH / N2O4 | — | Wikipedia |
| RD-275M | Energomash | 1,832 kN | 316s | 1,070 kg | 175 | UDMH / N2O4 | — | Wikipedia |
| RD-254 | Energomash | 1,720 kN | 328s | — | — | UDMH / N2O4 | — | Wikipedia |
| AJ-60A 3D | Aerojet Rocketdyne | 1,688 kN | 274s | 44,000 kg | 3.9 | HTPB | Atlas V 411, Atlas V 421, Atlas V 431, Atlas V 511, Atlas V 521, Atlas V 531, Atlas V 541, Atlas V 551 | Wikipedia |
| GEM 63 3D | Northrop Grumman | 1,688 kN | 274s | 24,948 kg | 6.9 | HTPB | — | Wikipedia |
| NK-33 | Kuznetsov | 1,680 kN | 331s | 1,240 kg | 138 | RP-1 / LOX | — | Wikipedia |
| NK-33A (AJ26-62) 3D | JSC Kuznetsov | 1,638 kN | 331s | 1,222 kg | 137 | RP-1 / LOX | Antares 110, Antares 120, Antares 130 | Wikipedia |
| RD-275 | NPO Energomash | 1,630 kN | 316s | — | — | UDMH / N2O4 | Proton-K, Proton-K/Briz-M, Proton-K/DM, Proton-K/DM-2, UR-500, UR-500K, UR-500K/Blok D | Wikipedia |
| RD-276 3D | NPO Energomash | 1,630 kN | 316s | — | — | UDMH / N2O4 | Proton-M, Proton-M/Briz-M | Wikipedia |
| RD-253 | Energomash | 1,630 kN | 316s | 1,080 kg | 154 | UDMH / N2O4 | — | Wikipedia |
| LE-9 3D | Mitsubishi, JAXA | 1,471 kN | 426s | 2,400 kg | 62.5 | LH2 / LOX | H3-22L, H3-22S, H3-24L, H3-24W, H3-30S | Wikipedia |
| Vulcain 2 3D | Snecma | 1,359 kN | 429s | 1,800 kg | 77 | LH2 / LOX | Ariane 5ECA, Ariane 5ECA+, Ariane 5ES, Ariane 5ES/ATV | Wikipedia |
| YF-100 3D | AALPT | 1,340 kN | 335s | 1,700 kg | 80 | RP-1 / LOX | Chang Zheng 12, Chang Zheng 12B, Chang Zheng 5, Chang Zheng 5/YZ-2, Chang Zheng 5B, Chang Zheng 6, Chang Zheng 6A, Chang Zheng 7, Chang Zheng 7A, Chang Zheng 8 | Wikipedia |
| Vulcain 2.1 3D | ArianeGroup | 1,324 kN | 433s | 2,000 kg | 68 | LH2 / LOX | Ariane 62, Ariane 64 | Wikipedia |
| J-2X 3D | Pratt & Whitney Rocketdyne | 1,307 kN | 448s | 2,470 kg | 55 | LH2 / LOX | — | Wikipedia |
| Zefiro 40 | Avio | 1,304 kN | 295s | 39,700 kg | 3.4 | HTPB | Vega C | Wikipedia |
| Aeon-R | Relativity Space | 1,240 kN | — | — | — | CH4 / LOX | — | Wikipedia |
| Zefiro 23 | Avio | 1,197 kN | 287s | 26,891 kg | 4.5 | HTPB | Vega | Wikipedia |
| RS-2200 | Rocketdyne | 1,180 kN | 439s | — | — | LH2 / LOX | — | Wikipedia |
| Vulcain HM-60 | Snecma | 1,140 kN | 431s | 1,300 kg | 69 | LH2 / LOX | Ariane 5G, Ariane 5G+, Ariane 5GS | Wikipedia |
| LE-7A 3D | Mitsubishi, JAXA | 1,098 kN | 440s | 1,800 kg | 63 | LH2 / LOX | H-IIA 202, H-IIA 204, H-IIB | Wikipedia |
| LE-7 | Mitsubishi, NASDA | 1,078 kN | 446s | 1,714 kg | 64 | LH2 / LOX | H-II | Wikipedia |
| RS-27A 3D | Rocketdyne | 1,054 kN | 316s | 1,027 kg | 94 | RP-1 / LOX | — | Wikipedia |
| J-2 3D | Rocketdyne | 1,033 kN | 421s | 1,788 kg | 60 | LH2 / LOX | Saturn IB, Saturn V | Wikipedia |
| RD-107A 3D | NPO Energomash | 1,020 kN | 320s | 1,190 kg | 72 | RP-1 / LOX | Soyuz-2-1A, Soyuz-2-1A Fregat, Soyuz-2-1B, Soyuz-2-1B Fregat, Soyuz-FG, Soyuz-ST-A, Soyuz-ST-B, Soyuz-U | Wikipedia |
| RD-117 | NPO Energomash | 1,000 kN | 315s | 1,190 kg | 72 | RP-1 / LOX | — | Wikipedia |
| XRS-2200 | Rocketdyne | 1,000 kN | 436s | — | — | LH2 / LOX | — | Wikipedia |
| RD-108A 3D | NPO Energomash | 992 kN | 320s | 1,278 kg | 65 | RP-1 / LOX | Soyuz-2-1A, Soyuz-2-1A Fregat, Soyuz-2-1B, Soyuz-2-1B Fregat, Soyuz-FG, Soyuz-ST-A, Soyuz-ST-B, Soyuz-U | Wikipedia |
| Merlin Vacuum 1D 3D | SpaceX | 981 kN | 348s | 490 kg | 194 | RP-1 / LOX | Falcon 9, Falcon Heavy | Wikipedia |
| RD-118 | NPO Energomash | 980 kN | 315s | 1,278 kg | 64 | RP-1 / LOX | — | Wikipedia |
| Merlin 1D FT 3D | SpaceX | 914 kN | 311s | 470 kg | 183 | RP-1 / LOX | Falcon 9, Falcon Heavy | Wikipedia |
| Archimedes 3D | Rocket Lab | 890 kN | 366s | 500 kg | 178 | CH4 / LOX | Neutron | Wikipedia |
| RD-120K | Yuzhnoye | 853.2 kN | 330s | 1,080 kg | 81 | RP-1 / LOX | — | Wikipedia |
| RD-120 | Yuzhmash | 833.6 kN | 350s | 1,125 kg | 76 | RP-1 / LOX | — | Wikipedia |
| RD-801 | Pivdenne / Pivdenmash | 818 kN | 338s | — | — | RP-1 / LOX | — | Wikipedia |
| TQ-12 3D | Landspace | 806 kN | 323s | 1,471 kg | 56 | CH4 / LOX | Zhuque-2, Zhuque-2E | Wikipedia |
| Viking 4B | Snecma | 805 kN | 295s | 826 kg | 99 | UH 25 / N2O4 | Ariane 2, Ariane 3, Ariane 40, Ariane 42L, Ariane 42P, Ariane 44L, Ariane 44P | Wikipedia |
| Vikas 3D | LPSC | 804 kN | 293s | 634 kg | 75 | UDMH / N2O4 | GSLV Mk I, GSLV Mk II, GSLV Mk III, LVM3, PSLV, PSLV-CA, PSLV-DL, PSLV-QL, PSLV-XL | Wikipedia |
| KRE-075 Vacuum | KARI / Hanwha Aerospace | 788 kN | 315s | — | — | Jet A-1 / LOX | — | Wikipedia |
| BE-3U 3D | Blue Origin | 765 kN | 445s | 1,550 kg | 90 | LH2 / LOX | New Glenn 7x2, New Shepard | Wikipedia |
| Viking 5C 3D | Snecma | 758 kN | 278s | 826 kg | 94 | UH 25 / N2O4 | Ariane 40, Ariane 42L, Ariane 42P, Ariane 44L, Ariane 44P | Wikipedia |
| YF-25 | AALPT | 755 kN | 289s | — | — | UDMH / N2O4 | Chang Zheng 2F, Chang Zheng 3B, Chang Zheng 3C | Wikipedia |
| Viking 6 | Snecma | 750 kN | 281s | 826 kg | 93 | UH 25 / N2O4 | Ariane 42L, Ariane 44L | Wikipedia |
| YF-22C | AALPT | 742 kN | 303s | — | — | UDMH / N2O4 | Chang Zheng 2F, Chang Zheng 3A, Chang Zheng 3B, Chang Zheng 3C, Chang Zheng 4B, Chang Zheng 4C | Wikipedia |
| YF-22B | AALPT | 742 kN | 303s | — | — | UDMH / N2O4 | Chang Zheng 2C, Chang Zheng 3, Chang Zheng 4 | Wikipedia |
| YF-22D | AALPT | 742 kN | 309s | — | — | UDMH / N2O4 | Chang Zheng 2D | Wikipedia |
| YF-22E | AALPT | 742 kN | 310s | — | — | UDMH / N2O4 | — | Wikipedia |
| KRE-075 | KARI / Hanwha Aerospace | 735.5 kN | 299s | — | — | Jet A-1 / LOX | — | Wikipedia |
| Viking 4 | Snecma | 713 kN | 295s | 826 kg | 88 | UDMH / N2O4 | Ariane 1 | Wikipedia |
| YF-77 3D | AALPT | 700 kN | 430s | 2,600 kg | 28 | LH2 / LOX | Chang Zheng 5, Chang Zheng 5/YZ-2, Chang Zheng 5B | Wikipedia |
| Viking 2 | Snecma | 690 kN | 281s | 776 kg | 91 | UDMH / N2O4 | Ariane 1 | Wikipedia |
| TR-106 | TRW | 650 kN | — | — | — | LH2 / LOX | — | Wikipedia |
| RD-0210 | KBKhA | 582 kN | 327s | 566 kg | 105 | UDMH / N2O4 | — | Wikipedia |
| RD-0213 | KBKhA | 582 kN | 327s | 550 kg | 108 | UDMH / N2O4 | — | Wikipedia |
| RD-0206 | KBKhA | 575.5 kN | 326s | — | — | UDMH / N2O4 | — | Wikipedia |
| RD-0208 | KBKhA | 570 kN | 326s | 540 kg | 108 | UDMH / N2O4 | — | Wikipedia |
| RD-0203 | KBKhA | 559 kN | 311s | 381 kg | 150 | UDMH / N2O4 | — | Wikipedia |
| Merlin 1C 3D | SpaceX | 556 kN | 304s | 630 kg | 96 | RP-1 / LOX | — | Wikipedia |
| Merlin Vacuum 1C | SpaceX | 411 kN | 342s | 630 kg | 70 | RP-1 / LOX | — | Wikipedia |
| NERVA 3D | LANL | 334 kN | 800s | 10,430 kg | 3 | LH2 | — | Wikipedia |
| NewtonThree | Virgin Orbit | 326.82 kN | — | — | — | RP-1 / LOX | LauncherOne | Wikipedia |
| RD-0124 3D | KBKhA | 298.17 kN | 359s | 480 kg | 63 | RP-1 / LOX | Angara A5, Angara A5/Persei, Angara-1.2, Soyuz-2-1A, Soyuz-2-1A Fregat, Soyuz-2-1B, Soyuz-2-1B Fregat, Soyuz-5, Soyuz-ST-A, Soyuz-ST-B | Wikipedia |
| RD-0110 | Voronezh Mechanical Plant (KBKhA) | 298 kN | 325s | 408.5 kg | 74 | RP-1 / LOX | — | Wikipedia |
| Zefiro 9A | Avio | 296 kN | 296s | 10,000 kg | 3 | HTPB | Vega, Vega C | Wikipedia |
| Gamma 8 | Bristol Siddeley | 243 kN | 265s | 435 kg | 57 | RP-1 / H2O2 | Black Arrow | Wikipedia |
| Reaver 1 3D | Firefly Aerospace | 213.4 kN | 295s | 127 kg | 171 | RP-1 / LOX | Alpha | Wikipedia |