H-IIA 2022
H-II familyMitsubishi Heavy IndustriesRetired
The H-IIA rocket family is an expendable launch system operated by Mitsubishi Heavy Industries for the Japan Aerospace Exploration Agency. The liquid fuelled rocket has been used to launch satellites, lunar spacecraft and planetary science craft.
Specifications
- Height
- 53 m
- Diameter
- 4 m
- Launch mass
- 316 t
- Stages
- 2
- GTO capacity
- 4,500 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
100%success rate3 of 3
0failuresincluding partial failures
3success streakcurrent
First flight February 26, 2005 · latest September 14, 2007
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for H-IIA flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2005 | 1 | 0 | 1 |
| 2006 | 1 | 0 | 1 |
| 2007 | 1 | 0 | 1 |