Delta 5920-8

E817842

Delta 5920-8 was a variant of the Delta expendable launch vehicle used by NASA to place the COBE satellite into orbit for cosmological observations.

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Statements (46)

Predicate Object
instanceOf Delta rocket variant
expendable launch vehicle
configurationCode 5920-8
countryOfOrigin United States of America
surface form: United States
fairingDiameter 2.4 meters
8 feet
family Delta 5000 series NERFINISHED
firstStage Extended Long Tank Thor NERFINISHED
Thor first stage
firstStageEngine RS-27 NERFINISHED
launchCustomer NASA Goddard Space Flight Center NERFINISHED
launchDate 1989-11-18
launches uncrewed payloads
launchOutcome success
launchSite Space Launch Complex 2W NERFINISHED
Vandenberg Air Force Base NERFINISHED
launchVehicleRole scientific research support
launchYear 1989
manufacturer McDonnell Douglas NERFINISHED
missionType astrophysics mission support
cosmology mission support
notableFor launching COBE to study cosmic microwave background
operator NASA
United States Air Force
partOf Delta rocket family NERFINISHED
payload COBE NERFINISHED
payloadMassClass low Earth orbit payload
payloadType cosmology observatory
program Delta launch vehicle program
propulsionType liquid and solid propulsion
reusability non-reusable
secondStage Delta-K NERFINISHED
secondStageEngine AJ10-118K NERFINISHED
stages three-stage with boosters
status retired
strapOnBoosters 9 solid rocket boosters
strapOnBoosterType Castor 4 NERFINISHED
targetOrbit Sun-synchronous-like orbit
low Earth orbit
thirdStage Star 48B NERFINISHED
thirdStageType solid rocket motor
usedBy NASA NERFINISHED
usedFor orbital launch
scientific satellite launch
usedToLaunch COBE NERFINISHED
Cosmic Background Explorer NERFINISHED

Referenced by (2)

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

COBE Differential Microwave Radiometer experiment launchVehicle Delta 5920-8
subject surface form: COBE Differential Microwave Radiometer