H-II rocket family

E424233

expendable launch system launch vehicle family

The H-II rocket family is a series of Japanese liquid-fueled expendable launch vehicles developed by JAXA and Mitsubishi Heavy Industries for placing satellites and spacecraft into orbit.

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All labels observed (5)

Label	Occurrences
H-II	3
H-II rocket family canonical	2
H-II rocket	1
H-II series	1
H‑II rocket	1

Statements (45)

Predicate	Object
instanceOf	expendable launch system ⓘ launch vehicle family ⓘ
abbreviation	H-II rocket family self-linksurface differs ⓘ surface form: H-II
agency	Japan Aerospace Exploration Agency ⓘ
boosters	solid rocket boosters ⓘ
countryOfOrigin	Japan ⓘ
designFeature	cryogenic first stage ⓘ cryogenic second stage ⓘ
developer	Japan Aerospace Exploration Agency ⓘ Japan Aerospace Exploration Agency ⓘ surface form: National Space Development Agency of Japan
firstFlightDate	1994-02-03 ⓘ
firstFlightSite	Tanegashima Space Center ⓘ Tanegashima Space Center ⓘ surface form: Yoshinobu Launch Complex
firstFlightVehicle	H-II rocket family self-linksurface differs ⓘ surface form: H-II
firstStageOxidizer	liquid oxygen ⓘ
firstStagePropellant	liquid hydrogen ⓘ
fuelType	cryogenic propellant ⓘ
launchCapability	geostationary transfer orbit ⓘ low Earth orbit ⓘ
launchesFrom	Tanegashima Space Center ⓘ
launchType	orbital launch vehicle ⓘ
launchVehicleVariant	H-II rocket family self-linksurface differs ⓘ surface form: H-II H-IIA launch vehicle ⓘ surface form: H-IIA H-IIB launch vehicle ⓘ surface form: H-IIB
manufacturer	Mitsubishi Heavy Industries ⓘ
market	commercial launch market ⓘ institutional launch market ⓘ
notablePayload	Himawari weather satellites ⓘ communications satellites ⓘ
operator	Japan Aerospace Exploration Agency ⓘ surface form: JAXA Mitsubishi Heavy Industries ⓘ
precededBy	H-I rocket ⓘ
primaryMission	commercial satellite launch ⓘ government satellite launch ⓘ
propulsionType	liquid-fueled ⓘ
stageConfiguration	two-stage ⓘ
status	retired ⓘ
successor	H-IIA launch vehicle ⓘ surface form: H-IIA H-IIB launch vehicle ⓘ surface form: H-IIB
technologyOrigin	domestically developed core stage ⓘ
upperStageOxidizer	liquid oxygen ⓘ
upperStagePropellant	liquid hydrogen ⓘ
usedFor	satellite launch ⓘ spacecraft launch ⓘ
usedInProgram	Japanese space program ⓘ

Referenced by (8)

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

H-IIB launch vehicle → family → H-II rocket family ⓘ

Tropical Rainfall Measuring Mission → launchVehicle → H-II rocket family ⓘ

this entity surface form: H-II rocket

H-II rocket family → abbreviation → H-II rocket family self-linksurface differs ⓘ

this entity surface form: H-II

H-II rocket family → firstFlightVehicle → H-II rocket family self-linksurface differs ⓘ

this entity surface form: H-II

H-II rocket family → launchVehicleVariant → H-II rocket family self-linksurface differs ⓘ

this entity surface form: H-II

LE-5B → usedOnVehicleFamily → H-II rocket family ⓘ

this entity surface form: H-II series

Engineering Test Satellite series → launchVehicleUsed → H-II rocket family ⓘ

this entity surface form: H‑II rocket

H-2B → family → H-II rocket family ⓘ