SA-10
E899998
SA-10 is a specific aircraft (or spacecraft) designation known primarily as the final vehicle flown by the pilot or mission labeled S-I.
Statements (37)
| Predicate | Object |
|---|---|
| instanceOf |
Saturn I launch vehicle
ⓘ
space launch vehicle ⓘ |
| alsoKnownAs |
AS-103 (in some Apollo-related designations)
NERFINISHED
ⓘ
Saturn I SA-10 NERFINISHED ⓘ |
| configuration | Saturn I Block II NERFINISHED ⓘ |
| countryOfOperator |
United States of America
ⓘ
surface form:
United States
|
| firstStageEngineCount | 8 ⓘ |
| firstStageEngineType | H-1 engine ⓘ |
| firstStageType | S-I first stage ⓘ |
| flightNumberInProgram | 10 ⓘ |
| followedBy | SA-201 ⓘ |
| is |
final Saturn I launch
ⓘ
final Saturn I vehicle flown ⓘ |
| launchDate |
1965-07-30
ⓘ
30 July 1965 ⓘ |
| launchMassCategory | medium-lift launch vehicle ⓘ |
| launchOutcome | success ⓘ |
| launchSite |
Cape Kennedy Air Force Station Launch Complex 37B
NERFINISHED
ⓘ
LC-37B NERFINISHED ⓘ |
| launchVehicleFor | Pegasus 3 NERFINISHED ⓘ |
| manufacturer |
Chrysler (first stage)
NERFINISHED
ⓘ
Douglas Aircraft Company (second stage) NERFINISHED ⓘ |
| missionType |
orbital launch
ⓘ
satellite deployment ⓘ |
| operatedBy | NASA ⓘ |
| orbitTypeAchieved | low Earth orbit ⓘ |
| partOf | Saturn I program NERFINISHED ⓘ |
| payload | Pegasus 3 micrometeoroid-detection satellite NERFINISHED ⓘ |
| precededBy | SA-9 ⓘ |
| primaryObjective |
continued evaluation of Saturn I performance
ⓘ
test of Pegasus 3 satellite ⓘ |
| programPhase | test and development phase of Apollo infrastructure ⓘ |
| propulsionType | liquid-fueled ⓘ |
| rocketFamily | Saturn NERFINISHED ⓘ |
| secondStageType | S-IV second stage ⓘ |
| status | retired ⓘ |
| usedForProgram | Apollo program development NERFINISHED ⓘ |
Referenced by (2)
Full triples — surface form annotated when it differs from this entity's canonical label.