CE-20
E822848
CE-20 is a cryogenic rocket engine developed by the Indian Space Research Organisation (ISRO) to power the upper stage of its heavy-lift launch vehicles.
All labels observed (1)
| Label | Occurrences |
|---|---|
| CE-20 canonical | 2 |
Statements (46)
| Predicate | Object |
|---|---|
| instanceOf | cryogenic rocket engine ⓘ |
| application |
deep space mission injection
ⓘ
satellite launch ⓘ |
| associatedAgency | Department of Space (India) NERFINISHED ⓘ |
| belongsToProgram | Indian cryogenic engine program NERFINISHED ⓘ |
| burnTime | long-duration upper-stage burn ⓘ |
| category | rocket engine ⓘ |
| chamberPressure | approximately 60 bar ⓘ |
| countryOfOrigin | India ⓘ |
| designedFor |
GSLV Mk III
NERFINISHED
ⓘ
LVM3 NERFINISHED ⓘ |
| designGoal |
enable higher payload capacity to GTO
ⓘ
provide indigenous cryogenic upper-stage capability ⓘ |
| developer | Indian Space Research Organisation NERFINISHED ⓘ |
| developmentAgency | Liquid Propulsion Systems Centre NERFINISHED ⓘ |
| engineCycle | gas-generator cycle ⓘ |
| firstFlightVehicle | LVM3-D3 NERFINISHED ⓘ |
| firstOperationalUse | GSLV Mk III / LVM3 missions NERFINISHED ⓘ |
| fuel | liquid hydrogen ⓘ |
| gimbalCapability | yes ⓘ |
| ignitionSystem | pyrotechnic igniter ⓘ |
| intendedStage | upper stage ⓘ |
| manufacturer | Liquid Propulsion Systems Centre NERFINISHED ⓘ |
| missionProfile | injection into GTO and higher orbits ⓘ |
| operatingEnvironment | vacuum ⓘ |
| organization | ISRO NERFINISHED ⓘ |
| oxidizer | liquid oxygen ⓘ |
| propellantCombination | LOX-LH2 ⓘ |
| propellantFeedSystem | turbopump-fed ⓘ |
| propellantType | cryogenic ⓘ |
| propulsionType | chemical rocket ⓘ |
| relatedEngine | CE-7.5 ⓘ |
| restartCapability | single-start ⓘ |
| role | upper-stage propulsion for heavy-lift rockets ⓘ |
| specificImpulseVacuum | approximately 442 s ⓘ |
| status | operational ⓘ |
| technologyOrigin | indigenously developed in India ⓘ |
| testFacility | ISRO Propulsion Complex, Mahendragiri NERFINISHED ⓘ |
| thrustVacuum | approximately 200 kN ⓘ |
| thrustVectorControl | gimballed engine mount ⓘ |
| usedBy | ISRO launch vehicles NERFINISHED ⓘ |
| usedFor |
communication satellite launches
ⓘ
geosynchronous transfer orbit missions ⓘ heavy-lift launch vehicles ⓘ |
| usedIn |
C25 stage
ⓘ
LVM3 upper stage NERFINISHED ⓘ |
Referenced by (2)
Full triples — surface form annotated when it differs from this entity's canonical label.