SA-204

E914994

SA-204 was a Saturn IB launch vehicle used by NASA during the Apollo program, notably associated with the ill-fated Apollo 1 mission.

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Statements (47)

Predicate Object
instanceOf Saturn IB launch vehicle
expendable launch system
alsoKnownAs AS-204
associatedWithEvent Apollo 1 cabin fire
countryOfOrigin United States of America
surface form: United States
firstStage S-IB stage NERFINISHED
firstStageEngineType Rocketdyne H-1 NERFINISHED
followedBy SA-205
hardwareReassignmentReason cancellation of crewed Apollo 1 flight after fire
height 224 ft
68 m
launchDate 1968-01-22
launchMass ~1,300,000 lb
~590,000 kg
launchOutcome success
launchSite Cape Kennedy Air Force Station Launch Complex 37B NERFINISHED
LC-37B NERFINISHED
launchTimeUTC 1968-01-22T22:48:08Z
launchVehicleSerialNumber SA-204
liftoffThrust ~1,600,000 lbf
~7,100 kN
manufacturer Chrysler Corporation Space Division NERFINISHED
Douglas Aircraft Company NERFINISHED
Rocketdyne NERFINISHED
missionName Apollo 5 NERFINISHED
missionObjective test of Lunar Module ascent and descent engines in Earth orbit
missionPayload Apollo Lunar Module test article LM-1 NERFINISHED
missionType uncrewed Earth-orbital test flight
numberOfFirstStageEngines 8
numberOfSecondStageEngines 1 GENERATED
operator NASA
orbitType low Earth orbit
originallyAssignedToMission Apollo 1 GENERATED
partOf Apollo program NERFINISHED
precededBy SA-203
programPhase early Apollo Earth-orbital test phase
propellantFirstStage RP-1 kerosene
liquid oxygen
propellantSecondStage liquid hydrogen
liquid oxygen
rocketFamily Saturn I family NERFINISHED
Saturn IB NERFINISHED
secondStage S-IVB stage NERFINISHED
secondStageEngineType Rocketdyne J-2 NERFINISHED
stageCount 2
status retired
usedForMission Apollo 5 NERFINISHED

Referenced by (1)

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