Apollo CSM Block I
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
View of Spacecraft 012 Command Module during pre-shipping operations
Credit: NASA
American manned spacecraft. The Apollo Command Service Module was the spacecraft developed by NASA in the 1960's as a standard spacecraft for earth and lunar orbit missions.
Block I command service modules, which lacked forward docking tunnels and hatches, never flew manned after the Apollo 204 fire killed its crew on the pad.
Crew Size: 3. Habitable Volume: 6.17 m3. RCS total impulse: 3,774 kgf-sec. Spacecraft delta v: 2,804 m/s (9,199 ft/sec). Electric System: 690.00 kWh. Electric System: 6.30 average kW.
Related
- Family
- Manned spacecraft
- Country
- USA
- Engines
- AJ10-137
- Launch Vehicles
- Saturn I
- Propellants
- N2O4/UDMH
- Agency
- NASA, North American
Photo Gallery
Apollo CSM Block 1
Apollo Spacecraft 012 hoisted to top of gantry at Pad 34
Credit: NASA
Apollo CSM Block 1
Apollo Spacecraft 012 hoisted to top of gantry at Pad 34
Credit: NASA
Apollo CSM Block 1
Close-up view of Apollo Spacecraft 012 Command Module after flash fire
Credit: NASA
Apollo CSM Block 1
Apollo Spacecraft 017 moved for mating with Saturn V launch vehicle
Credit: NASA
Apollo CSM Block 1
Apollo Spacecraft 020 Command Module readied for mating with Service Module
Credit: NASA
Apollo 203
Credit: Manufacturer Image
