Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:book |
gptkb:AJ10-118K_engine
|
| gptkbp:boosters |
4
|
| gptkbp:configuration |
7420-10C
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
2.44 meters
|
| gptkbp:fairingDiameter |
10 feet
|
| gptkbp:family |
gptkb:Delta_II
|
| gptkbp:launchSite |
gptkb:Cape_Canaveral_SLC-17A
gptkb:Vandenberg_SLC-2W |
| gptkbp:length |
38.9 meters
|
| gptkbp:manufacturer |
gptkb:Boeing
gptkb:McDonnell_Douglas |
| gptkbp:massToGTO |
2,170 kg
|
| gptkbp:notableMission |
gptkb:Jason-1
gptkb:Mars_Odyssey |
| gptkbp:numberOfStages |
gptkb:RS-27A_engine
|
| gptkbp:payloadToLEO |
5,900 kg
|
| gptkbp:propellantFirstStage |
gptkb:Aerozine_50/N2O4
RP-1/LOX |
| gptkbp:solidRocketBoosters |
gptkb:GEM-40
|
| gptkbp:status |
retired
|
| gptkbp:thirdPlace |
none
|
| gptkbp:usedFor |
commercial payloads
NASA missions satellite launches |
| gptkbp:bfsParent |
gptkb:ICESat-2
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta II 7420-10C
|