Function | Heavy-lift launch vehicle |
---|---|
Manufacturer | United Launch Alliance |
Country of origin | United States |
Cost per launch | US$110 million (starting)[1] |
Size | |
Height | Standard: 61.6 m (202 ft) Long: 67.3 m (221 ft)[2] |
Diameter | 5.4 m (18 ft)[3] |
Mass | 546,700 kg (1,205,300 lb) |
Stages | 2 |
Capacity | |
Payload to LEO | |
Orbital inclination | 28.7° |
Mass | 27,200 kg (60,000 lb)[4] |
Payload to GTO | |
Orbital inclination | 27° |
Mass | 15,300 kg (33,700 lb)[4] |
Payload to GEO | |
Mass | 7,000 kg (15,000 lb)[4] |
Payload to TLI | |
Mass | 12,100 kg (26,700 lb)[4] |
Launch history | |
Status | Operational |
Launch sites |
|
Total launches | 2 |
Success(es) | 2 |
First flight | 8 January 2024[6] |
Boosters – GEM-63XL | |
No. boosters | 0, 2, 4, or 6[7] |
Height | 21.98 m (865.3 in) |
Diameter | 1.62 m (63.7 in) |
Empty mass | 4,521 kg (9,966 lb) |
Gross mass | 53,030 kg (116,920 lb) |
Propellant mass | 47,853 kg (105,497 lb) |
Maximum thrust | 2,061 kN (463,249 lbf) each |
Specific impulse | 280.3 s (2.749 km/s) |
Burn time | 87.3 seconds[8] |
Propellant | AP / HTPB / Al |
First stage – Vulcan | |
Height | 33.3 m (109 ft) |
Diameter | 5.4 m (18 ft) |
Powered by | 2 × BE-4 |
Maximum thrust | 4,900 kN (1,100,000 lbf) |
Burn time | 299 seconds[9][10] |
Propellant | LOX / CH4 |
Second stage – Centaur V | |
Height | 11.7 m (38 ft) |
Diameter | 5.4 m (18 ft) |
Powered by | 2 × RL10[11] |
Maximum thrust | 212 kN (48,000 lbf)[12] |
Specific impulse | 453.8 s (4.450 km/s)[12] |
Propellant | LOX / LH2 |
Vulcan Centaur is a heavy-lift launch vehicle created and operated by United Launch Alliance (ULA). It is a two-stage-to-orbit launch vehicle consisting of the Vulcan first stage and the Centaur second stage. It replaces ULA's Atlas V and Delta IV rockets. It is principally designed for the National Security Space Launch (NSSL) program, which launches satellites for U.S. intelligence agencies and the Defense Department, but ULA believes it will also be able to price missions low enough to attract commercial launches.
ULA began developing the Vulcan in 2014, largely to compete with SpaceX's Falcon 9 and to comply with a Congressional requirement to stop using the Russian-made RD-180 engine that powered the Atlas V. The first flight of the Vulcan Centaur was initially slated for 2019, but was delayed multiple times by developmental problems with its new BE-4 first-stage engine and the Centaur second-stage.[13]
The Vulcan Centaur had a near perfect first launch on 8 January 2024 carrying the Peregrine lunar lander, the first mission of NASA's Commercial Lunar Payload Services program. It made its second launch, a NSSL certification flight, on 4 October 2024, which achieved a perfect orbital insertion, despite the nozzle on one of the GEM-63XL solid rocket boosters falling off which led to reduced, asymmetrical thrust.
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