Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:chamberPressure |
60 bar
|
| gptkbp:countryOfOrigin |
gptkb:India
|
| gptkbp:cycle |
gas-generator
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:firstFlight |
2014
|
| gptkbp:fuelType |
liquid hydrogen
|
| https://www.w3.org/2000/01/rdf-schema#label |
ME20
|
| gptkbp:length |
2.8 m
|
| gptkbp:manufacturer |
gptkb:ISRO
|
| gptkbp:numberOfEnginesPerStage |
1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
cryogenic
|
| gptkbp:specificImpulseVacuum |
443 s
|
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
200 kN
|
| gptkbp:usedFor |
upper stage
|
| gptkbp:usedIn |
gptkb:GSLV_Mk_III
|
| gptkbp:bfsParent |
gptkb:Royal_British_Legion_Village,_Aylesford
gptkb:Ditton gptkb:Aylesford gptkb:Larkfield gptkb:New_Hythe gptkb:Aylesford,_Kent,_England gptkb:Aylesford,_England |
| gptkbp:bfsLayer |
7
|