CM-017
E584966
CM-017 is the Apollo 4 command module, an uncrewed early Apollo spacecraft used by NASA to test the Saturn V rocket and reentry systems in 1967.
Statements (32)
| Predicate | Object |
|---|---|
| instanceOf |
Apollo command module
ⓘ
spacecraft ⓘ uncrewed spacecraft ⓘ |
| associatedRocket | Saturn V SA-501 NERFINISHED ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| crewCapacity | 3 (design capacity) ⓘ |
| crewed | no ⓘ |
| era | 1960s ⓘ |
| flightStatus | flown ⓘ |
| heatShieldType | ablative heat shield ⓘ |
| launchComplex | Launch Complex 39A NERFINISHED ⓘ |
| launchDate | 1967-11-09 ⓘ |
| launchSite | Kennedy Space Center NERFINISHED ⓘ |
| launchVehicle | Saturn V NERFINISHED ⓘ |
| manufacturer | North American Aviation NERFINISHED ⓘ |
| missionDesignation | Apollo 4 command module NERFINISHED ⓘ |
| missionNumberInProgram | first Saturn V test flight ⓘ |
| missionOutcome | success ⓘ |
| missionType | test flight ⓘ |
| operatedBy | NASA ⓘ |
| partOf | Apollo 4 NERFINISHED ⓘ |
| program | Apollo program NERFINISHED ⓘ |
| recovered | yes ⓘ |
| reentrySpeedCategory | lunar-return-simulated reentry ⓘ |
| reentryTestObjective |
guidance and control during reentry
ⓘ
heat shield performance ⓘ structural integrity during high-speed reentry ⓘ |
| reentryType | Earth atmospheric reentry ⓘ |
| spaceAgency | National Aeronautics and Space Administration NERFINISHED ⓘ |
| testedConfiguration | Block I Apollo command module NERFINISHED ⓘ |
| usedFor |
test of Apollo reentry systems
ⓘ
test of Saturn V launch vehicle ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.