Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:alternativeName |
gptkb:Proton_8K82
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Vladimir_Chelomey
|
| gptkbp:diameter |
4.1 m
|
| gptkbp:engineType |
liquid-fueled
|
| gptkbp:firstFlight |
1965-07-10
|
| gptkbp:fuelType |
UDMH
|
| https://www.w3.org/2000/01/rdf-schema#label |
UR-500
|
| gptkbp:launchSite |
gptkb:Baikonur_Cosmodrome
|
| gptkbp:length |
49.1 m
|
| gptkbp:manufacturer |
gptkb:OKB-52
|
| gptkbp:mass |
620,000 kg
|
| gptkbp:notableMission |
gptkb:Zond_5
gptkb:Zond_6 |
| gptkbp:numberOfStages |
2
|
| gptkbp:oxidizer |
N2O4
|
| gptkbp:payloadToLEO |
12,200 kg
|
| gptkbp:purpose |
later used as a space launch vehicle
originally designed as a heavy ICBM |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Proton_rocket
|
| gptkbp:usedFor |
gptkb:Zond_program
|
| gptkbp:bfsParent |
gptkb:Proton_rocket
|
| gptkbp:bfsLayer |
6
|