H-IIA 212
Launch vehicle · Japan
Original archive entry. The text, images and links below are kept as they were written.
Japanese orbital launch vehicle. This version uses two core stages side-by-side in an asymmetric configuration, supplemented by two SRB-A solid rocket boosters.
LEO Payload: 17,280 kg (38,090 lb) to a 300 km orbit at 30.40 degrees. Payload: 7,500 kg (16,500 lb) to a GTO.
Related
- Family
- orbital launch vehicle
- Country
- Japan
- Engines
- LE-5B engine, LE-7A
- Agency
- Mitsubishi