Properties (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
launch vehicle
|
| gptkbp:designedBy |
Convair
|
| gptkbp:diameter |
3.05 meters
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:firstFlight |
1960-12-18
1978-05-30 |
| gptkbp:height |
30.5 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Atlas-Agena
|
| gptkbp:launchSite |
gptkb:Vandenberg_Space_Force_Base
gptkb:Cape_Canaveral_Space_Force_Station |
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:notableFeature |
gptkb:Gemini_missions
gptkb:Mariner_2 Viking 1 Lunar Orbiter 1 |
| gptkbp:numberOfStudents |
2
|
| gptkbp:payloadCapacity |
1,500 kg to low Earth orbit
|
| gptkbp:productionYears |
1960-1978
|
| gptkbp:succeededBy |
90%
|
| gptkbp:successor |
gptkb:Atlas_Centaur
|
| gptkbp:usedFor |
satellite launch
|
| gptkbp:weight |
150,000 kg
|