LE-7A

E410446

The LE-7A is a Japanese liquid-fueled rocket engine used to power the core stage of the H-IIA family of launch vehicles.

Try in SPARQL Jump to: Surface forms Statements Referenced by

All labels observed (2)

Label Occurrences
LE-7A canonical 3
LE-7 1

Statements (45)

Predicate Object
instanceOf liquid-fueled rocket engine
abbreviationOf Liquid Engine-7A
application core stage propulsion
belongsToProgram H-IIA program
H-IIB launch vehicle
surface form: H-IIB program
chamberPressure_MPa about 12
combustionChambers 1
countryOfOrigin Japan
designedBy Mitsubishi Heavy Industries
developer Japan Aerospace Exploration Agency
engineCycle staged combustion cycle
engineType main engine
firstFlightVehicle H-IIA launch vehicle
surface form: H-IIA 202
firstFlightYear 2001
gimbalCapability_deg about 6
launchVehicleFamily H-IIA launch vehicle
surface form: H-IIA

H-IIB launch vehicle
surface form: H-IIB
manufacturer Mitsubishi Heavy Industries
nozzles 1
oxidizer liquid oxygen
oxidizerRich true
predecessor LE-7A self-linksurface differs
surface form: LE-7
propellantFeedSystem turbopump-fed
propellantType liquid hydrogen
liquid oxygen
propulsionType cryogenic
reliabilityImprovedFrom LE-7
specificImpulseSeaLevel_s about 360
specificImpulseVacuum_s about 440
stageApplication first stage
status operational
successor LE-9
throttleCapability limited
thrustSeaLevel_kN about 890
thrustVacuum_kN about 1110
usedByAgency Japan Aerospace Exploration Agency
surface form: JAXA
usedByCountry Japan
usedFor orbital launch
satellite deployment
spacecraft launch
usedForMissionType geostationary transfer orbit missions
interplanetary missions
sun-synchronous orbit missions
usedIn H-IIA launch vehicle
H-IIB launch vehicle

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.

LE-7A predecessor LE-7A self-linksurface differs
this entity surface form: LE-7
H-2B firstStageEngine LE-7A
LE-9 predecessor LE-7A