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AS-201
Sign in to saveAS-201 (Also known as SA-201, Apollo 1-A, or Apollo 1 prior to the 1967 pad fire, flown February 26, 1966, was the first uncrewed test flight of an entire production Block I Apollo command and service module and the Saturn IB launch vehicle. The spacecraft consisted of the second Block I command module and the first Block I service module. The suborbital flight was a partially successful demonstration of the service propulsion system and the reaction control systems of both modules, and successfully demonstrated the capability of the command module's heat shield to survive re-entry from low Ea
Key facts
- Spaceflight.name
- AS-201
- Spaceflight.image
- AS-201 launch.jpg
- Spaceflight.image_caption
- Launch of AS-201, the first flight of the Apollo spacecraft and Saturn IB launch vehicle
- Spaceflight.mission_type
- Suborbital test flight
- Spaceflight.operator
- NASA
- Spaceflight.mission_duration
- 37 minutes, 19.7 seconds
- Spaceflight.spacecraft
- Apollo CSM-009
- Spaceflight.manufacturer
- North American Aviation
- Spaceflight.launch_date
- UTC
- Spaceflight.launch_rocket
- Saturn IB SA-201
- Spaceflight.launch_site
- Cape Kennedy LC-34
- Spaceflight.landing_date
- UTC
- Spaceflight.landing_site
- South Atlantic Ocean
- Spaceflight.previous_mission
- AS-105
- Spaceflight.next_mission
- Apollo 2
- Spaceflight.programme
- Apollo program
via Wikipedia infobox
Article
13 sectionsContents
- Vehicle configuration
- Spacecraft
- Launch vehicle
- Objectives
- Preparation for flight
- Flight
- Launch attempt
- Flight
- Problems
- Capsule location
- See also
- References
- External links
AS-201 (Also known as SA-201, Apollo 1-A, or Apollo 1 prior to the 1967 pad fire, flown February 26, 1966, was the first uncrewed test flight of an entire production Block I Apollo command and service module and the Saturn IB launch vehicle. The spacecraft consisted of the second Block I command module and the first Block I service module. The suborbital flight was a partially successful demonstration of the service propulsion system and the reaction control systems of both modules, and successfully demonstrated the capability of the command module's heat shield to survive re-entry from low Earth orbit.
==Vehicle configuration==