Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:capacity |
785 kg
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:derivedFrom |
gptkb:V-2_rocket
|
| gptkbp:designer |
gptkb:Sergei_Korolev
|
| gptkbp:developedBy |
gptkb:OKB-1
|
| gptkbp:diameter |
1.65 m
|
| gptkbp:elevation |
85 km
|
| gptkbp:enteredService |
1950
|
| gptkbp:firstFlight |
1948
|
| https://www.w3.org/2000/01/rdf-schema#label |
R-1 rocket
|
| gptkbp:launchMass |
13,400 kg
|
| gptkbp:length |
14.1 m
|
| gptkbp:manufacturer |
gptkb:Soviet_Union
|
| gptkbp:numberBuilt |
about 100
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
ethanol
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:R-2_rocket
|
| gptkbp:usedFor |
scientific research
military testing |
| gptkbp:bfsParent |
gptkb:Kapustin_Yar
gptkb:Tsygan |
| gptkbp:bfsLayer |
6
|