سفینه فرماندهی و خدمات آپولو
Sign in to saveAlso known as CSM, Command and Service Module
component of the United States Apollo spacecraft
Key facts
- Manufacturer
- North American Aviation
- Designer
- Maxime Faget
- Country of origin
- United States
- Operator
- NASA
- Applications
- Crewed cislunar flight and lunar orbit , Skylab crew shuttle, Apollo–Soyuz Test Project
- Spacecraft type
- Capsule
- Launch mass
- 32,390 lb (14,690 kg) Earth orbit, 63,500 lb (28,800 kg) Lunar
- Dry mass
- 26,300 lb (11,900 kg)
- Payload capacity
- 2,320 lb (1,050 kg)
- Volume
- 218 ft (6.2 m )
- Power
- 3 × 1.4 kW, 30 V DC fuel cells
- Batteries
- 3 × 40 ampere-hour silver zinc battery
- Regime
- Low Earth orbit , Cislunar space , Lunar orbit
- Design life
- 14 days
- Length
- 36.2 ft (11.0 m)
- Diameter
- 12.8 ft (3.9 m)
- Status
- Retired
- Maiden launch
- February 26, 1966 ; 60 years ago ( February 26, 1966 ) ( AS-201 )
via Wikipedia infobox
Wikidata facts
- Subclass of
- crewed spacecraft
- Part of
- Apollo
- Operator
- NASA
- Country of origin
- United States
- Diameter
- 3.9
- Mass
- 1050
- Manufacturer
- Rockwell International
- Designed by
- Maxime Faget
- Image
- Apollo CSM lunar orbit.jpg
- Length
- 11
Show 7 more facts
- Commons category
- Apollo Command and Service Modules
- total produced
- 35
- volume as quantity
- 6.2
- maximum capacity
- 3
- space launch vehicle
- Saturn V
- service life
- 14
- native label
- Apollo Command and Service Module
Sources (1)
via Wikidata · CC0