Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.52 meters
|
| gptkbp:engineType |
gptkb:Bell_8096
|
| gptkbp:firstFlight |
1962
|
| gptkbp:lastFlight |
1987
|
| gptkbp:length |
6.3 meters
|
| gptkbp:manufacturer |
gptkb:Lockheed
|
| gptkbp:mass |
7,000 kg
|
| gptkbp:notableMission |
gptkb:Gemini_Agena_Target_Vehicle
gptkb:Corona_reconnaissance_satellites |
| gptkbp:numberBuilt |
over 360
|
| gptkbp:oxidizer |
inhibited red fuming nitric acid
|
| gptkbp:predecessor |
Agena-B upper stage
|
| gptkbp:propulsion |
unsymmetrical dimethylhydrazine
|
| gptkbp:status |
retired
|
| gptkbp:successor |
none
|
| gptkbp:thrust |
71 kN
|
| gptkbp:usedFor |
satellite launches
space probe launches military missions |
| gptkbp:usedOn |
gptkb:Atlas-Agena
gptkb:Titan_IIIB gptkb:Thor-Agena |
| gptkbp:bfsParent |
gptkb:Gemini_Agena_Target_Vehicle
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Agena-D upper stage
|