Delta 2914
E846914
Delta 2914 was a variant of the Delta expendable launch vehicle family used by NASA to place scientific satellites, including the International Ultraviolet Explorer, into orbit.
Statements (32)
| Predicate | Object |
|---|---|
| instanceOf |
Delta rocket variant
ⓘ
expendable launch system ⓘ |
| agencyUser | NASA Goddard Space Flight Center NERFINISHED ⓘ |
| coreStage | Thor-Delta first stage NERFINISHED ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| designLineage | Thor IRBM-derived launcher NERFINISHED ⓘ |
| era |
1970s
ⓘ
1980s ⓘ |
| family | Thor-Delta NERFINISHED ⓘ |
| launchCapability |
geosynchronous transfer orbit
ⓘ
low Earth orbit ⓘ |
| launchComplex | Launch Complex 17 NERFINISHED ⓘ |
| launchConfiguration | 2000-series Delta ⓘ |
| launchMethod | expendable ⓘ |
| launchSite | Cape Canaveral Air Force Station NERFINISHED ⓘ |
| launchVehicleRole | medium-lift launch vehicle ⓘ |
| manufacturer | McDonnell Douglas NERFINISHED ⓘ |
| notablePayload | International Ultraviolet Explorer NERFINISHED ⓘ |
| numberOfStages | 3 ⓘ |
| operatedBy | NASA ⓘ |
| partOf | Delta rocket family NERFINISHED ⓘ |
| propellantTypeFirstStage | RP-1/LOX ⓘ |
| propellantTypeSecondStage | Aerozine 50/N2O4 ⓘ |
| propellantTypeThirdStage | solid propellant ⓘ |
| status | retired ⓘ |
| strapOnBoosters | 9 Castor-2 solid rocket boosters ⓘ |
| successor | Delta 3000 series NERFINISHED ⓘ |
| thirdStage | Star-37D NERFINISHED ⓘ |
| upperStage | Delta second stage ⓘ |
| usedFor |
launching Earth-orbiting spacecraft
ⓘ
launching astronomical observatories ⓘ launching scientific satellites ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.