AKA: Service Module. Status: Operational 1964. Thrust: 97.86 kN (22,000 lbf). Gross mass: 24,523 kg (54,063 lb). Unfuelled mass: 6,110 kg (13,470 lb). Specific impulse: 314 s. Height: 7.56 m (24.80 ft). Diameter: 3.90 m (12.70 ft).
Structure: 1,910 kg (4,210 lb). Electrical Equipment: 1,200 kg (2,600 lb). RCS Coarse No x Thrust: 16 x 440 N. RCS specific impulse: 290 sec. RCS total impulse: 3,517 kgf-sec. Spacecraft delta v: 2,804 m/s (9,199 ft/sec). Electric System: 670.00 kWh. Electric System: 6.30 average kW.
Family: Manned spacecraft module. Country: USA. Spacecraft: Apollo CSM. Propellants: N2O4/UDMH. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
Search and Browse the WWW like it's 1997 | Search results from DuckDuckGo
HTML:
3.2
| Encoding:
UTF-8
| Version:
0.7.4