Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
3.7 m
|
| gptkbp:engine |
RD-58
|
| gptkbp:engineType |
liquid rocket engine
|
| gptkbp:family |
Blok-DM family
|
| gptkbp:firstFlight |
1974
|
| gptkbp:length |
6.3 m
|
| gptkbp:manufacturer |
gptkb:RSC_Energia
|
| gptkbp:mass |
17,000 kg
|
| gptkbp:numberOfEngines |
1
|
| gptkbp:propulsion |
kerosene
liquid oxygen |
| gptkbp:purpose |
orbital insertion
geostationary transfer orbit trans-lunar injection |
| gptkbp:status |
active
|
| gptkbp:successor |
Blok-DM-03
Blok-DM-2 |
| gptkbp:thrust |
83.4 kN
|
| gptkbp:usedBy |
gptkb:Soviet_space_program
gptkb:Russian_space_program gptkb:Roscosmos |
| gptkbp:usedFor |
interplanetary missions
lunar missions launching satellites |
| gptkbp:usedOn |
gptkb:Proton_rocket
gptkb:N1_rocket gptkb:Zenit_rocket |
| gptkbp:bfsParent |
gptkb:Raduga_satellites
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Blok-DM upper stage
|