Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
3.05 m
|
| gptkbp:engineType |
gptkb:Rocketdyne_engines
|
| gptkbp:failedFlights |
5
|
| gptkbp:firstFlight |
11 June 1957
|
| gptkbp:lastFlight |
3 June 1958
|
| gptkbp:launchMass |
109,000 kg
|
| gptkbp:length |
21.4 m
|
| gptkbp:manufacturer |
gptkb:Convair
|
| gptkbp:numberBuilt |
8
|
| gptkbp:numberOfStages |
1
|
| gptkbp:partOf |
gptkb:SM-65_Atlas_program
|
| gptkbp:propulsion |
liquid oxygen and RP-1
|
| gptkbp:purpose |
test vehicle for Atlas missile development
|
| gptkbp:range |
965 km
|
| gptkbp:status |
retired
|
| gptkbp:successfulFlights |
3
|
| gptkbp:successor |
gptkb:Atlas_B_missile
|
| gptkbp:usedBy |
gptkb:United_States_Air_Force
|
| gptkbp:bfsParent |
gptkb:Atlas_B_missile
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Atlas A missile
|