SA-2

E898866

SA-2 is a specific space mission or spacecraft designation associated with the S-I launch vehicle in the early U.S. space program.

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Observed surface forms (1)

Surface form Occurrences
SA-3 1

Statements (43)

Predicate Object
instanceOf Saturn I test flight
space mission
suborbital test flight
apogee approximately 105 kilometers
codename Project Highwater NERFINISHED
country United States of America
surface form: United States
firstStageEngines 8 H-1 engines
firstStagePropellants RP-1 kerosene
liquid oxygen
flightDuration about 15 minutes
followedBy SA-3
guidanceSystem inertial guidance
historicalSignificance contributed to development of Saturn launch vehicles used in Apollo program
early test of clustered-engine large launch vehicle
launchDate 1962-04-25
launchLocation Cape Canaveral, Florida NERFINISHED
launchMass approximately 500 metric tons
launchSite Cape Canaveral Air Force Station Launch Complex 34 NERFINISHED
LC-34 NERFINISHED
launchTimeUTC 1962-04-25T14:00:34Z
launchVehicle Saturn I NERFINISHED
launchVehicleConfiguration Block I Saturn I NERFINISHED
launchVehicleStage S-I first stage
missionObjective demonstrate high-altitude release of ballast water
simulate orbital payload mass using water ballast
test guidance and control systems
test propulsion system performance
test structural integrity of Saturn I first stage
missionType boilerplate payload test
developmental test flight
operator NASA Marshall Space Flight Center NERFINISHED
outcome first successful Project Highwater experiment
partOf Saturn I program NERFINISHED
early U.S. space program
payload boilerplate upper stages
water ballast
precededBy SA-1
program Saturn I NERFINISHED
projectName Project Highwater NERFINISHED
spaceAgency NASA
status success
waterBallastMass about 109000 liters of water
waterReleaseAltitude approximately 105 kilometers

Referenced by (2)

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

S-I usedInMission SA-2
S-I usedInMission SA-2
this entity surface form: SA-3