Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.52 m
|
| gptkbp:engineType |
gptkb:Bell_8096
|
| gptkbp:firstFlight |
1959
|
| https://www.w3.org/2000/01/rdf-schema#label |
Agena upper stage
|
| gptkbp:length |
6.3 m
|
| gptkbp:manufacturer |
gptkb:Lockheed_Corporation
|
| gptkbp:mass |
7,000 kg
|
| gptkbp:oxidizer |
inhibited red fuming nitric acid
|
| gptkbp:propulsion |
unsymmetrical dimethylhydrazine
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Centaur_upper_stage
|
| gptkbp:thrust |
16,000 lbf
|
| gptkbp:usedAs |
rocket upper stage
spacecraft bus |
| gptkbp:usedIn |
gptkb:Gemini_program
gptkb:Ranger_program gptkb:Mariner_program gptkb:Corona_reconnaissance_satellites gptkb:Lunar_Orbiter_program |
| gptkbp:bfsParent |
gptkb:satellite
|
| gptkbp:bfsLayer |
4
|