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.

All labels observed (1)

Label Occurrences
Delta 5920-8 canonical 5

How this entity was disambiguated

Statements (46)

Predicate Object
instanceOf Delta rocket variant
expendable launch vehicle
configurationCode 5920-8
countryOfOrigin United States
fairingDiameter 2.4 meters
8 feet
family Delta 5000 series
firstStage Extended Long Tank Thor
linked to: Thor-Able

Thor first stage
firstStageEngine RS-27
linked to: RS-27 rocket engine
launchCustomer NASA Goddard Space Flight Center
launchDate 1989-11-18
launches uncrewed payloads
launchOutcome success
launchSite Space Launch Complex 2W
Vandenberg Air Force Base
launchVehicleRole scientific research support
launchYear 1989
manufacturer McDonnell Douglas
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
payload COBE
payloadMassClass low Earth orbit payload
payloadType cosmology observatory
program Delta launch vehicle program
propulsionType liquid and solid propulsion
reusability non-reusable
secondStage Delta-K
linked to: Delta
secondStageEngine AJ10-118K
stages three-stage with boosters
status retired
strapOnBoosters 9 solid rocket boosters
strapOnBoosterType Castor 4
targetOrbit Sun-synchronous-like orbit
low Earth orbit
thirdStage Star 48B
thirdStageType solid rocket motor
usedBy NASA
usedFor orbital launch
scientific satellite launch
usedToLaunch COBE
Cosmic Background Explorer

How these facts were elicited

Referenced by (5)

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

COBE Differential Microwave Radiometer launchVehicle Delta 5920-8
1989-089A launchVehicle Delta 5920-8
Explorer 66 launchVehicle Delta 5920-8