Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:basedOn |
gptkb:V-2_rocket
|
| gptkbp:designer |
gptkb:Sergei_Korolev
|
| gptkbp:diameter |
1.65 m
|
| gptkbp:engineType |
RD-101
|
| gptkbp:enteredService |
1951
|
| gptkbp:exportedTo |
gptkb:China
|
| gptkbp:firstFlight |
1949
|
| gptkbp:guidanceSystem |
inertial
|
| https://www.w3.org/2000/01/rdf-schema#label |
R-2 missile
|
| gptkbp:launchWeight |
20,300 kg
|
| gptkbp:length |
17.7 m
|
| gptkbp:manufacturer |
gptkb:OKB-1
|
| gptkbp:notableFor |
sounding rocket (R-2A variant)
|
| gptkbp:notableVariant |
R-2A
|
| gptkbp:origin |
gptkb:Soviet_Union
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
600 km
|
| gptkbp:retired |
1959
|
| gptkbp:successor |
gptkb:R-5_missile
|
| gptkbp:usedBy |
gptkb:China
gptkb:Soviet_Union |
| gptkbp:warheadType |
conventional
|
| gptkbp:website |
gptkb:Kapustin_Yar
|
| gptkbp:bfsParent |
gptkb:Tactical_Missiles_Corporation
|
| gptkbp:bfsLayer |
5
|