Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:ChineseVariant |
gptkb:Dongfeng_1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:derivedFrom |
gptkb:V-2_rocket
|
| gptkbp:designer |
gptkb:Sergei_Korolev
|
| gptkbp:diameter |
1.65 m
|
| gptkbp:engineType |
piston engine
|
| gptkbp:enteredService |
1950
|
| gptkbp:exportedTo |
gptkb:China
|
| gptkbp:firstFlight |
1949
|
| https://www.w3.org/2000/01/rdf-schema#label |
R-2 rocket
|
| gptkbp:launchMass |
20,300 kg
|
| gptkbp:length |
17.7 m
|
| gptkbp:manufacturer |
gptkb:OKB-1
|
| gptkbp:notableFor |
first Soviet missile to carry animals in suborbital flights
|
| gptkbp:payload |
1,000 kg
|
| gptkbp:predecessor |
gptkb:R-1_rocket
|
| gptkbp:propulsion |
ethanol
liquid oxygen |
| gptkbp:range |
600 km
|
| gptkbp:retired |
1959
|
| gptkbp:successor |
gptkb:R-5_rocket
|
| gptkbp:usedBy |
gptkb:Soviet_Army
|
| gptkbp:website |
gptkb:Kapustin_Yar
|
| gptkbp:bfsParent |
gptkb:Kapustin_Yar
|
| gptkbp:bfsLayer |
6
|