Jupiter 246-B
Revision as of 20:29, 8 July 2016 by Lafayette1 (talk | contribs) (Created page with "{{Infobox rocket |image = |caption = |name = Jupiter 246-B |function = Manned launch vehicle |country-origin = United States |height = 362 ft |diameter =...")
| Function | Manned launch vehicle |
|---|---|
| Country of origin | United States |
| Size | |
| Height | 362 ft |
| Stages | 2 |
| Capacity | |
| Payload to LEO (241 km x 29°) |
|
| Associated rockets | |
| Family | SDLV |
| Comparable | National Launch System |
| Launch history | |
| Status | Active |
| Launch sites | LC-39, Kennedy Space Center |
| Notable payloads | Orion Crew Exploration Vehicle Altair Lunar Surface Access Module |
| Boosters (Stage 0) - Shuttle RSRM | |
| No boosters | 2 |
| Engines | 1 solid |
| Thrust | (sea level - vacuum) |
| Total thrust | (sea level - vacuum) |
| Specific impulse | 237.0 - 269.1 sec (sea level - vacuum) |
| Burn time | 123.8 sec |
| Fuel | APCP/PBAN |
| First Stage - Common core stage | |
| Engines | 4 SSME-Block-II |
| Thrust | (sea level - vacuum) |
| Specific impulse | 361.4 (SL) 452.2 sec (sea level - vacuum) |
| Burn time | 384.1 sec |
| Fuel | LOX/LH2 |
| Second Stage - Jupiter Upper Stage | |
| Engines | 6 RL10B-2 |
| Thrust | (vacuum) |
| Specific impulse | 459 sec (vacuum) |
| Burn time | 609.9 sec |
| Fuel | LOX/LH2 |
