H-IIA launch vehicle
E86314
The H-IIA launch vehicle is a Japanese expendable rocket system used primarily for satellite deployment and space exploration missions.
Observed surface forms (9)
| Surface form | Occurrences |
|---|---|
| H-IIA | 7 |
| H-IIA 202 | 3 |
| H-II rocket family | 1 |
| H-IIA 2024 | 1 |
| H-IIA 204 | 1 |
| H-IIA 222 | 1 |
| H-IIA 224 | 1 |
| H-IIA program | 1 |
| JAXA H-IIA program | 1 |
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
expendable launch vehicle
ⓘ
orbital launch vehicle ⓘ |
| abbreviation |
H-IIA launch vehicle
self-linksurface differs
ⓘ
surface form:
H-IIA
|
| agencyProgram |
H-IIA launch vehicle
self-linksurface differs
ⓘ
surface form:
JAXA H-IIA program
|
| boosterPropellantType | solid propellant ⓘ |
| coreStageEngine | LE-7A ⓘ |
| countryOfOrigin | Japan ⓘ |
| developer | Japan Aerospace Exploration Agency ⓘ |
| firstFlightDate | 2001-08-29 ⓘ |
| firstFlightLaunchSite | Tanegashima Space Center ⓘ |
| firstFlightPayload | LRE satellite ⓘ |
| launchConfiguration |
H-IIA launch vehicle
self-linksurface differs
ⓘ
surface form:
H-IIA 202
H-IIA 2022 ⓘ H-IIA launch vehicle self-linksurface differs ⓘ
surface form:
H-IIA 2024
H-IIA launch vehicle self-linksurface differs ⓘ
surface form:
H-IIA 204
H-IIA launch vehicle self-linksurface differs ⓘ
surface form:
H-IIA 222
H-IIA launch vehicle self-linksurface differs ⓘ
surface form:
H-IIA 224
|
| launchesNotablePayload |
Akatsuki Venus climate orbiter
ⓘ
BepiColombo mission ⓘ
surface form:
BepiColombo Mercury mission (JAXA contribution)
Engineering Test Satellite series ⓘ GOSAT greenhouse gases observation satellites ⓘ
surface form:
GOSAT greenhouse gases observing satellite
Hayabusa spacecraft ⓘ
surface form:
Hayabusa asteroid sample return mission
Himawari meteorological satellites ⓘ
surface form:
Himawari-8 weather satellite
Himawari meteorological satellites ⓘ
surface form:
Himawari-9 weather satellite
Ikaros solar sail ⓘ Martian Moons eXploration mission ⓘ QZSS Michibiki navigation satellites ⓘ |
| launchServiceProvider | Mitsubishi Heavy Industries ⓘ |
| launchSite | Tanegashima Space Center ⓘ |
| manufacturer | Mitsubishi Heavy Industries ⓘ |
| operator |
Japan Aerospace Exploration Agency
ⓘ
Mitsubishi Heavy Industries ⓘ |
| partOf |
H-IIA launch vehicle
self-linksurface differs
ⓘ
surface form:
H-II rocket family
|
| primaryLaunchComplex |
Tanegashima Space Center
ⓘ
surface form:
Yoshinobu Launch Complex
|
| propellantType |
liquid hydrogen
ⓘ
liquid oxygen ⓘ |
| retirementDate | 2024 ⓘ |
| stages | 2 ⓘ |
| status | retired ⓘ |
| successor | H3 launch vehicle ⓘ |
| upperStageEngine | LE-5B ⓘ |
| usedFor |
Earth observation satellites
ⓘ
communications satellites ⓘ interplanetary missions ⓘ navigation satellites ⓘ satellite deployment ⓘ space exploration missions ⓘ weather satellites ⓘ |
Referenced by (21)
Full triples — surface form annotated when it differs from this entity's canonical label.
this entity surface form:
H-IIA
this entity surface form:
JAXA H-IIA program
this entity surface form:
H-IIA 202
this entity surface form:
H-IIA 2024
this entity surface form:
H-IIA 204
this entity surface form:
H-IIA 222
this entity surface form:
H-IIA 224
this entity surface form:
H-IIA
subject surface form:
GOSAT
this entity surface form:
H-IIA
subject surface form:
GOSAT-2
this entity surface form:
H-IIA
this entity surface form:
H-IIA 202
subject surface form:
Hayabusa2
this entity surface form:
H-IIA 202
subject surface form:
SLIM
this entity surface form:
H-IIA
this entity surface form:
H-IIA
this entity surface form:
H-IIA
this entity surface form:
H-II rocket family
this entity surface form:
H-IIA program