Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:diameter |
1.56 m
|
| gptkbp:firstFlight |
2014
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:length |
2.1 m
|
| gptkbp:manufacturer |
gptkb:ISRO
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
cryogenic
|
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
75 kN
|
| gptkbp:usedIn |
gptkb:GSLV_Mk_II
GSLV-F05 GSLV-F09 GSLV-F10 GSLV-F11 GSLV-F12 GSLV-F13 GSLV-F14 |
| gptkbp:bfsParent |
gptkb:Liquid_Propulsion_Systems_Centre_(LPSC)
|
| gptkbp:bfsLayer |
6
|
| http://www.w3.org/2000/01/rdf-schema#label |
CE-7.5 cryogenic engine
|