H-IIA
Mitsubishi Heavy Industries developed H-IIA, a H-II vehicle operated by Mitsubishi Heavy Industries.
Specifications
- Height
- 53 m
- Diameter
- 4 m
- Mass
- 285000 kg
- Stages
- 2
- Thrust
- 2260 kN
- LEO payload
- 10000 kg
- First flight
- Aug 29, 2001
Manufacturer & operator
- Family
- H-II
- Variant
- 202
- Manufacturer
- Mitsubishi Heavy Industries
- Operator
- β
- Country
- Japan
Launch sites
- Tanegashima Space Center, Japan (35 launches)
Launch history
35 launches to date.
SUCCESSH-IIA 202 | GOSAT-GW (Ibuki GW)
SUCCESSH-IIA 202 | IGS Radar 8
SUCCESSH-IIA 202 | IGS Optical 8
SUCCESSH-IIA 202 | XRISM & SLIM
SUCCESSH-IIA 202 | IGS Radar 7
SUCCESSH-IIA 202 | QZS-1R
SUCCESSH-IIA 202 | JDRS-1
SUCCESSH-IIA 202 | Hope (Emirates Mars Mission)
SUCCESSH-IIA 202 | IGS Optical 7
SUCCESS