Minotaur V
Country of Origin: United States
Manufacturer: Orbital Sciences
Height: 24.56 m
Diameter: 2.67 m
Payload to LEO: (532kg to GTO, 342kg to TLI)
Total Mass: 89.373 tons
Launch Sites: Vandenberg, Wallops, Kodiak
First Flight: September 7, 2013
Last Flight: Active
Total Launches: 1
Successful Launches: 1
Minotaur V
| Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
|---|---|---|---|---|---|---|---|
| 1 (SR-118) | 2.67 m | Solid | Thiokol TU-903 | 83 s | 2200 kN | 248.9 s / ? | 50.0 / 4.31 tons |
| 2 (SR-119) | Solid | 54 s | 1365 kN | ? / 308.9 s | 27.67 / 3.18 tons | ||
| 3 (SR-120) | Solid | 62 s | 329 kN | ? / 299.9 s | 7.71 / 0.63 tons | ||
| 4 (Star-48BV) | Solid | TE-M-940-1 | 84.1 s | 64 kN | ? / 293.9 s | 2.15 / 0.14 tons | |
| 5 (Star-37FM) | HTPB | TE-M-783 | 63 s | 47.26 kN | ? / 289.8 s | 1147.4 kg / 81.5 kg |
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