Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:developedBy |
gptkb:ISRO
|
| gptkbp:diameter |
4 m
|
| gptkbp:engine |
CE-20
|
| gptkbp:firstFlight |
2017
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:length |
13.5 m
|
| gptkbp:mass |
56,500 kg
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
cryogenic
|
| gptkbp:status |
active
|
| gptkbp:thrust |
186 kN
|
| gptkbp:usedFor |
launching heavy payloads to GTO
|
| gptkbp:usedIn |
gptkb:GSLV_Mk_III
|
| gptkbp:bfsParent |
gptkb:Launch_Vehicle_Mark-3
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
C25 cryogenic stage
|