L110 liquid core stage
E889639
The L110 liquid core stage is a cryogenic rocket stage used in India’s GSLV Mk III launch vehicle, providing the main liquid propulsion for its ascent.
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
launch vehicle core stage
ⓘ
rocket stage ⓘ |
| burnTime | approximately 200 seconds ⓘ |
| controlSystem | hydraulic gimbal actuators ⓘ |
| countryOfOrigin | India ⓘ |
| developedBy |
LPSC
NERFINISHED
ⓘ
Liquid Propulsion Systems Centre NERFINISHED ⓘ |
| diameter | 4 meters ⓘ |
| engineArrangement | twin-engine ⓘ |
| engineType | Vikas engine NERFINISHED ⓘ |
| firstFlightVehicle | GSLV Mk III D1 NERFINISHED ⓘ |
| firstFlightYear | 2017 ⓘ |
| fuel |
UDMH
ⓘ
unsymmetrical dimethylhydrazine ⓘ |
| guidance | gimballed engines for thrust vector control ⓘ |
| isPartOf |
GSLV Mk III launch vehicle
NERFINISHED
ⓘ
LVM3 launch vehicle NERFINISHED ⓘ |
| launchPad | Second Launch Pad, SDSC NERFINISHED ⓘ |
| launchSite | Satish Dhawan Space Centre NERFINISHED ⓘ |
| launchVehicleConfiguration | two S200 boosters plus L110 core plus C25 upper stage ⓘ |
| launchVehicleFamily | Geosynchronous Satellite Launch Vehicle Mark III NERFINISHED ⓘ |
| length | approximately 21 meters ⓘ |
| lowerStage | S200 solid rocket booster ⓘ |
| manufacturer |
ISRO Propulsion Complex
NERFINISHED
ⓘ
Indian Space Research Organisation NERFINISHED ⓘ |
| missionProfilePhase | ascent phase main propulsion ⓘ |
| numberOfEngines | 2 ⓘ |
| operator | Indian Space Research Organisation ⓘ |
| oxidizer |
N2O4
ⓘ
nitrogen tetroxide ⓘ |
| propellantMass |
110 metric tons
ⓘ
110000 kilograms ⓘ |
| propellantType | hypergolic propellant ⓘ |
| propulsionType | liquid propulsion ⓘ |
| reusability | expendable ⓘ |
| stageRole |
core stage
ⓘ
second stage of GSLV Mk III ⓘ |
| status | operational ⓘ |
| structureMaterial | aluminium alloy ⓘ |
| successorTo | GS2 stage of GSLV Mk II NERFINISHED ⓘ |
| thrustAtSeaLevel | about 1600 kilonewtons ⓘ |
| thrustInVacuum | about 1800 kilonewtons ⓘ |
| upperStage | C25 cryogenic upper stage ⓘ |
| usedFor |
geostationary transfer orbit missions
ⓘ
high-energy orbit missions ⓘ orbital launch ⓘ |
| usedInRocket |
GSLV Mk III
NERFINISHED
ⓘ
LVM3 NERFINISHED ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.