Command Module C-020
E915629
Command Module C-020 was the crew capsule used on NASA’s uncrewed Apollo 6 test flight, designed to validate systems for future manned lunar missions.
Statements (47)
| Predicate | Object |
|---|---|
| instanceOf |
Apollo command module
ⓘ
crew capsule ⓘ spacecraft component ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| crewCapacity | 3 astronauts ⓘ |
| crewStatusOnMission | uncrewed ⓘ |
| designedFor |
crewed lunar landing architecture
ⓘ
lunar mission program ⓘ |
| hasComponentType |
control panels
ⓘ
crew couches ⓘ environmental control system ⓘ parachute recovery system ⓘ reaction control system ⓘ |
| heatShieldType | ablative heat shield ⓘ |
| historicalEra | Space Race NERFINISHED ⓘ |
| launchDate | 1968-04-04 ⓘ |
| launchSite | Kennedy Space Center Launch Complex 39A ⓘ |
| manufacturer | North American Rockwell NERFINISHED ⓘ |
| missionDesignation | Apollo 6 command module NERFINISHED ⓘ |
| missionNumber | Apollo 6 NERFINISHED ⓘ |
| missionOutcome | partial success ⓘ |
| missionType | uncrewed test flight ⓘ |
| operator | NASA ⓘ |
| partOf | Apollo 6 NERFINISHED ⓘ |
| predecessorInProgram | Apollo 4 command module C-017 NERFINISHED ⓘ |
| primaryPurpose |
test command module performance on Saturn V
ⓘ
validate systems for future crewed Apollo missions ⓘ |
| programGoalContext | enable future crewed lunar orbit and landing missions ⓘ |
| programPhase | Apollo test phase ⓘ |
| recovered | true ⓘ |
| recoveryAgency | U.S. Navy NERFINISHED ⓘ |
| recoveryMethod | splashdown in the Pacific Ocean ⓘ |
| reentryType | Earth atmospheric reentry ⓘ |
| shape | blunt-body cone ⓘ |
| spaceAgencyProgram | NASA Apollo lunar landing program NERFINISHED ⓘ |
| spacecraftRole | crew capsule ⓘ |
| spacecraftSeries | Block II Apollo command module ⓘ |
| spaceProgram | Apollo program NERFINISHED ⓘ |
| testedSystems |
command module propulsion and control
ⓘ
communications systems ⓘ electrical power systems ⓘ guidance and navigation systems ⓘ structural integrity under Saturn V launch loads ⓘ thermal protection during reentry ⓘ |
| usedFor | qualification of Block II command module design ⓘ |
| usedOnLaunchVehicle |
AS-502
ⓘ
Saturn V NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.