Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:basedOn |
gptkb:V-2_rocket
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Sergei_Korolev
|
| gptkbp:diameter |
1.65 m
|
| gptkbp:engineType |
liquid-propellant rocket engine
|
| gptkbp:enteredService |
1950
|
| gptkbp:firstFlight |
1948
|
| gptkbp:guidanceSystem |
inertial
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soviet R-1 missile
|
| gptkbp:launchWeight |
13,400 kg
|
| gptkbp:length |
14.1 m
|
| gptkbp:manufacturer |
gptkb:NII-88
|
| gptkbp:platform |
mobile transporter erector launcher
|
| gptkbp:propulsion |
liquid-fueled
|
| gptkbp:range |
270 km
|
| gptkbp:retired |
1953
|
| gptkbp:successor |
gptkb:R-2_missile
|
| gptkbp:usedBy |
gptkb:Soviet_Army
|
| gptkbp:warheadType |
785 kg
|
| gptkbp:website |
gptkb:Kapustin_Yar
|
| gptkbp:bfsParent |
gptkb:German_V-2_program
|
| gptkbp:bfsLayer |
6
|