SA-9

E905384

SA-9 is a mission or operation designation associated with the S-I rocket stage program in early U.S. spaceflight development.

All labels observed (1)

Label Occurrences
SA-9 canonical 1

How this entity was disambiguated

Statements (47)

Predicate Object
instanceOf Saturn I mission ⓘ
uncrewed spaceflight mission ⓘ
agencyProgram NASA Apollo program ⓘ
linked to: Apollo program
apogee approximately 740 kilometers ⓘ
country United States ⓘ
crew uncrewed ⓘ
dataUse design of Apollo spacecraft micrometeoroid protection ⓘ
designation Saturn-Apollo 9 ⓘ
era early 1960s space race ⓘ
firstStageEngines 8 H-1 engines ⓘ
firstStagePropellant RP-1 and liquid oxygen ⓘ
inclination approximately 31.7 degrees ⓘ
launchDate 1965-02-16 ⓘ
launchOutcome success ⓘ
launchPad LC-37B ⓘ
launchSite Cape Canaveral, Florida ⓘ
linked to: Cape Canaveral

Cape Kennedy Air Force Station Launch Complex 37B ⓘ
launchTimeUTC 14:37:02 ⓘ
launchVehicle Saturn I ⓘ
launchVehicleStage S-I first stage ⓘ
S-IV second stage ⓘ
linked to: S-IV
micrometeoroidExperiment Pegasus deployable wing detectors ⓘ
missionDuration Pegasus 1 operational for several years in orbit ⓘ
missionOutcome success ⓘ
missionType Apollo boilerplate test ⓘ
suborbital test flight ⓘ
nextMission SA-10 ⓘ
notableFeature early validation of Apollo spacecraft structural design ⓘ
first Pegasus micrometeoroid satellite launch ⓘ
operator NASA ⓘ
orbitalPeriod approximately 97 minutes ⓘ
orbitType low Earth orbit ⓘ
partOf Apollo program test flights ⓘ
linked to: Apollo program

Saturn I program ⓘ
linked to: Saturn I
payload Apollo boilerplate command and service module BP-16 ⓘ
Pegasus 1 micrometeoroid detection satellite ⓘ
payloadMass approximately 16,965 kilograms ⓘ
perigee approximately 502 kilometers ⓘ
previousMission SA-8 ⓘ
primaryObjective deploy Pegasus 1 for micrometeoroid environment studies ⓘ
test Saturn I Block II vehicle performance ⓘ
programSequence ninth Saturn I flight ⓘ
rocketConfiguration Saturn I Block II ⓘ
linked to: Saturn I
secondaryObjective test Apollo boilerplate spacecraft and launch escape system ⓘ
secondStageEngines 6 RL10A-3 engines ⓘ
secondStagePropellant liquid hydrogen and liquid oxygen ⓘ
spacecraftType Apollo boilerplate spacecraft ⓘ

How these facts were elicited

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

S-I → usedInMission → SA-9 ⓘ