LE-9

E418620

The LE-9 is a next-generation liquid hydrogen–liquid oxygen rocket engine developed by Japan’s JAXA and Mitsubishi Heavy Industries for the core stage of the H3 launch vehicle, emphasizing high efficiency and cost-effective, reliable operation.

All labels observed (1)

Label Occurrences
LE-9 canonical 3

How this entity was disambiguated

Statements (45)

Predicate Object
instanceOf liquid-propellant rocket engine ⓘ
rocket engine ⓘ
agency JAXA ⓘ
application Japanese commercial launches ⓘ
Japanese governmental missions ⓘ
chamberPressure_bar about 100 ⓘ
countryOfOrigin Japan ⓘ
cycleSubtype expander bleed–like simplified staged combustion ⓘ
cycleType staged combustion cycle ⓘ
designFeature gimbal capability for thrust vector control ⓘ
hydrogen-rich staged combustion ⓘ
integrated engine and nozzle structure ⓘ
simplified turbomachinery ⓘ
single-shaft turbopump configuration ⓘ
designGoal cost reduction ⓘ
ease of manufacturing ⓘ
high efficiency ⓘ
high reliability ⓘ
developer JAXA ⓘ
Japan Aerospace Exploration Agency ⓘ
firstHotFireTests 2010s ⓘ
industrialPartner Mitsubishi Heavy Industries ⓘ
intendedStage core stage ⓘ
intendedVehicle H3 launch vehicle ⓘ
manufacturer Mitsubishi Heavy Industries ⓘ
mixtureRatio_OxToFuel about 6 ⓘ
nozzleExpansionRatio about 60 ⓘ
numberOfEnginesOnCoreStage 2 or 3 depending on configuration ⓘ
oxidizer liquid oxygen ⓘ
predecessor LE-7A ⓘ
program H3 Launch Vehicle Program ⓘ
linked to: H3 launch vehicle
propellant liquid hydrogen ⓘ
propellantFeedSystem turbopump-fed ⓘ
propellantType cryogenic ⓘ
specificImpulseSeaLevel_s about 360 ⓘ
specificImpulseVacuum_s about 425 ⓘ
status in development ⓘ
test phase ⓘ
thrustSeaLevel_kN about 1100 ⓘ
thrustVacuum_kN about 1500 ⓘ
usedOn H3-22 configuration ⓘ
H3-24 configuration ⓘ
uses interplanetary mission support via H3 ⓘ
orbital launch ⓘ
satellite launch ⓘ

How these facts were elicited

Referenced by (3)

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