Service Module 017
E584965
Service Module 017 was the Apollo service module used on the uncrewed Apollo 4 test flight to validate the Saturn V launch vehicle and Apollo spacecraft systems.
Statements (31)
| Predicate | Object |
|---|---|
| instanceOf |
Apollo service module
ⓘ
spacecraft component ⓘ |
| associatedMissionNumber | Apollo 4 (AS-501) NERFINISHED ⓘ |
| associatedWithLaunchVehicle | Saturn V SA-501 NERFINISHED ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| crewStatus | uncrewed ⓘ |
| designedFor | lunar mission-capable Apollo spacecraft ⓘ |
| era | 1960s ⓘ |
| flightDesignation | CSM-017 Service Module NERFINISHED ⓘ |
| launchCountry |
United States of America
ⓘ
surface form:
United States
|
| launchSite | Kennedy Space Center Launch Complex 39A ⓘ |
| launchVehicleValidated | Saturn V NERFINISHED ⓘ |
| manufacturer | North American Aviation NERFINISHED ⓘ |
| missionObjective |
validate Apollo spacecraft systems performance
ⓘ
validate Saturn V launch vehicle performance ⓘ |
| missionType | uncrewed test flight ⓘ |
| operatedBy | NASA Manned Spacecraft Center NERFINISHED ⓘ |
| partOf | Apollo 4 NERFINISHED ⓘ |
| program | Apollo program NERFINISHED ⓘ |
| relatedProgram | Saturn V development program ⓘ |
| role | service module for Apollo Command and Service Module stack ⓘ |
| spaceAgency | NASA ⓘ |
| spacecraftConfiguration | Apollo Command and Service Module NERFINISHED ⓘ |
| spacecraftSystemsValidated | Apollo spacecraft systems ⓘ |
| spacecraftType | Apollo Block I service module NERFINISHED ⓘ |
| status | retired ⓘ |
| usedFor |
electrical power system testing in flight
ⓘ
propulsion system testing in flight ⓘ structural testing in flight ⓘ thermal control system testing in flight ⓘ |
| usedOnMission | Apollo 4 NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.