Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:developedBy |
gptkb:Liquid_Propulsion_Systems_Centre
|
| gptkbp:diameter |
1.56 m
|
| gptkbp:firstFlight |
2017
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:gimbalRange |
+/- 5 degrees
|
| gptkbp:length |
2.05 m
|
| gptkbp:manufacturer |
gptkb:ISRO
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
cryogenic
|
| gptkbp:specificImpulseVacuum |
443 seconds
|
| gptkbp:status |
in service
|
| gptkbp:successor |
CE-7.5 engine
|
| gptkbp:thrustVacuum |
200 kN
|
| gptkbp:usedFor |
gptkb:upper_stage
|
| gptkbp:usedIn |
gptkb:Gaganyaan
gptkb:Chandrayaan-2 gptkb:LVM3 gptkb:Chandrayaan-3 gptkb:GSLV_Mk_III OneWeb launches |
| gptkbp:bfsParent |
gptkb:Liquid_Propulsion_Systems_Centre_(LPSC)
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
CE-20 cryogenic engine
|