Rocket Engine Family Tree
The world's major rocket engines organized top-down: first by country, then by engine family, down to individual models with propellant, combustion cycle and thrust. Expand a country, then a family, to trace each lineage — from the 1957 RD-107 to SpaceX's full-flow Raptor.
6 countries · 18 families · 33 engine models · curated from public manufacturer and reference data
United States6 families · 12 models▸
Merlin · SpaceXGas-generator RP-1/LOX family powering every Falcon flight; the highest-flight-rate rocket engines ever built.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| Merlin 1C | RP-1 / LOX | Gas generator | 480 kN | Falcon 9 v1.0 | Retired |
| Merlin 1D | RP-1 / LOX | Gas generator | 845 kN | Falcon 9, Falcon Heavy (first stage) | Active |
| Merlin 1D Vacuum | RP-1 / LOX | Gas generator | 934 kN | Falcon 9 / Heavy (second stage) | Active |
Raptor · SpaceXFull-flow staged-combustion methane family for Starship — the first engine of its cycle to fly.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| Raptor 1 | CH4 / LOX | Full-flow staged combustion | 1,850 kN | Starship prototypes | Retired |
| Raptor 2 | CH4 / LOX | Full-flow staged combustion | 2,300 kN | Starship (Block 1) | Active |
| Raptor 3 | CH4 / LOX | Full-flow staged combustion | 2,700 kN | Starship (Block 2+) | Active |
RS-25 · Aerojet RocketdyneStaged-combustion hydrolox main engine of the Space Shuttle, now flying on SLS.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| RS-25 (SSME) | LH2 / LOX | Staged combustion | 1,860 kN | Space Shuttle | Retired |
| RS-25E | LH2 / LOX | Staged combustion | 2,000 kN | SLS (expendable production unit) | Active |
F-1 · RocketdyneThe most powerful single-chamber liquid engine ever flown — five lifted each Saturn V.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| F-1 | RP-1 / LOX | Gas generator | 6,770 kN | Saturn V (S-IC) | Retired |
| F-1A | RP-1 / LOX | Gas generator | 8,000 kN | Never flown (Saturn V growth study) | Retired |
RL10 · Aerojet RocketdyneExpander-cycle hydrolox upper-stage engine in continuous production since the 1960s.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| RL10A/B/C variants | LH2 / LOX | Expander | 110 kN | Centaur, Delta IV upper stage | Active |
BE-4 · Blue OriginOxygen-rich staged-combustion methane engine flying on Vulcan and New Glenn.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| BE-4 | CH4 / LOX | Oxygen-rich staged combustion | 2,400 kN | Vulcan, New Glenn | Active |
Russia3 families · 5 models▸
RD-107 · Energomash / Kuznetsov lineageThe Soyuz engine family — the most-flown rocket engines in history, in service since 1957.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| RD-107 / RD-108 | RP-1 / LOX | Oxygen-rich staged combustion | 810 kN | Soyuz (boosters / core) | Active |
RD-170 · EnergomashThe most powerful liquid-propellant engine family ever built; scaled down into the RD-180 and RD-191.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| RD-170 / RD-171 | RP-1 / LOX | Oxygen-rich staged combustion | 7,250 kN | Energia, Zenit | Retired |
| RD-180 | RP-1 / LOX | Oxygen-rich staged combustion | 3,830 kN | Atlas V | Retired |
| RD-191 | RP-1 / LOX | Oxygen-rich staged combustion | 1,920 kN | Angara | Active |
NK-33 · KuznetsovClosed-cycle kerosene engines built for the Soviet N1 moon rocket, flown decades later.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| NK-15 / NK-33 | RP-1 / LOX | Oxygen-rich staged combustion | 1,510 kN | N1; NK-33 later flown on Soyuz-2.1v | Retired |
China4 families · 8 models▸
YF-100 · AALPTChina's oxygen-rich staged-combustion kerosene workhorse for the Long March 5/6/7/8/10 generation.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| YF-100 | RP-1 / LOX | Oxygen-rich staged combustion | 1,200 kN | Long March 5, 6, 7, 8 | Active |
| YF-100K | RP-1 / LOX | Oxygen-rich staged combustion | 1,300 kN | Long March 10 (crewed lunar program) | Active |
YF-75 · AALPTUpper-stage hydrolox family; the YF-75D added expander-cycle restart capability.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| YF-75 | LH2 / LOX | Gas generator | 78 kN | Long March 3A/3B/3C upper stage | Active |
| YF-75D | LH2 / LOX | Expander | 88 kN | Long March 5, 7A upper stage | Active |
YF-20 · AALPTHypergolic gas-generator family that powered the Long March 2/3/4 series for five decades.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| YF-20 / YF-21 | UDMH / N2O4 | Gas generator | 700 kN | Long March 2, 3, 4 series | Active |
Tianque (TQ) · LandSpaceGas-generator methane family behind the first methane rocket to reach orbit (Zhuque-2) and the reusable Zhuque-3.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| TQ-12 | CH4 / LOX | Gas generator | 670 kN | Zhuque-2 | Active |
| TQ-12B | CH4 / LOX | Gas generator | 780 kN | Zhuque-3 (first stage) | Active |
| TQ-15A | CH4 / LOX | Gas generator (vacuum) | 850 kN | Zhuque-2/3 second stage (vacuum thrust) | Active |
Europe2 families · 3 models▸
Vulcain · ArianeGroupGas-generator hydrolox main stage engine of Ariane 5 and Ariane 6.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| Vulcain 1 / 2 | LH2 / LOX | Gas generator | 1,000 kN | Ariane 5 | Retired |
| Vulcain 2.1 | LH2 / LOX | Gas generator | 1,140 kN | Ariane 6 | Active |
Vinci · ArianeGroupRestartable expander-cycle hydrolox upper-stage engine for Ariane 6.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| Vinci | LH2 / LOX | Expander | 180 kN | Ariane 6 upper stage | Active |
Japan1 family · 2 models▸
LE-7 / LE-9 · MHI / JAXAJapan's hydrolox main engines: staged-combustion LE-7A on H-IIA/B, expander-bleed LE-9 on H3.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| LE-7A | LH2 / LOX | Staged combustion | 1,100 kN | H-IIA, H-IIB | Retired |
| LE-9 | LH2 / LOX | Expander bleed | 1,470 kN | H3 | Active |
India2 families · 3 models▸
Vikas · ISRO / LPSCHypergolic gas-generator family derived from the Viking engine, flown on PSLV, GSLV and LVM3.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| Vikas 1 / 2 / 4 | UDMH / N2O4 | Gas generator | 800 kN | PSLV, GSLV, LVM3 | Active |
CE · ISRO / LPSCIndia's cryogenic hydrolox upper-stage engines, developed after the 1990s technology denial.▸
| Engine | Propellant | Cycle | Thrust | Used on | Status |
|---|
| CE-7.5 | LH2 / LOX | Staged combustion | 75 kN | GSLV Mk II upper stage | Active |
| CE-20 | LH2 / LOX | Gas generator | 200 kN | LVM3 upper stage | Active |
Engine parameters are approximate, compiled from public manufacturer fact sheets and reference sources. See our in-depth engine articles for detailed analysis of the Merlin/Raptor, RD-107→RD-170, YF-100 and RS-25 families.