Apollo 6

E267325

Apollo 6 was the second and final uncrewed test flight of NASA’s Saturn V rocket, launched in 1968 to validate the vehicle for subsequent crewed Apollo missions.

All labels observed (1)

Label Occurrences
Apollo 6 canonical 4

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf Apollo mission
test flight
uncrewed spaceflight
apoapsis 222,000 kilometers (planned)
countryOfOrigin United States of America
surface form: United States
crew none
failureEvent S-IC first stage longitudinal oscillations (pogo)
S-II second stage engine shutdowns
S-IVB third stage failure to restart
isFinalUncrewedSaturnVTest true
isUncrewed true
landingDate 1968-04-04
landingSite Pacific Ocean
launchDate 1968-04-04
launchLocation Kennedy Space Center
Merritt Island
surface form: Merritt Island, Florida
launchSite Kennedy Space Center Launch Complex 39A
LC-39A
launchTimeUTC 1968-04-04T12:00:01Z
launchVehicle Saturn V
launchVehicleVariant Saturn V
surface form: Saturn V SA-502
missionDuration 09:57:20
missionDurationSeconds 35840
missionOutcome partial success
missionType Saturn V test flight
uncrewed lunar mission simulation
nextMission Apollo 7
operator NASA
orbitReference Earth orbit
partOf Apollo program
periapsis ~176 kilometers (planned)
previousMission Apollo 5
primaryObjective demonstrate Saturn V performance for translunar injection
validate Saturn V launch vehicle for crewed Apollo missions
programGoalContext enable crewed lunar landing before the end of the 1960s
recoveredBy United States Navy
surface form: U.S. Navy
recoveryShip USS Okinawa
reentrySpeed approximately 10.4 km/s (less than planned lunar-return speed)
resultingChange engine and control system design refinements for later Saturn V flights
modifications to Saturn V pogo suppression systems
secondaryObjective test Apollo Command and Service Module in high-speed reentry conditions
spaceAgency NASA
surface form: National Aeronautics and Space Administration
spacecraftComponent Command Module C-020
Apollo Lunar Module
surface form: Lunar Module Test Article (boilerplate) LM-2

Service Module SM-014
spacecraftType Block I Command and Service Module
status completed
usedForQualificationOf Saturn V
surface form: Saturn V for crewed Apollo missions
yearOfSpaceflight 1968

How these facts were elicited

Referenced by (4)

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

Apollo 7 precededBy Apollo 6
S-IC usedOnMission Apollo 6
J-2 usedDuringMission Apollo 6