Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
H-IIA 212
Part of H-2 Family
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.

AKA: H-2A 212. Status: In production. Payload: 17,280 kg (38,090 lb). Thrust: 6,400.00 kN (1,438,700 lbf). Gross mass: 406,000 kg (895,000 lb). Height: 52.50 m (172.20 ft). Diameter: 4.00 m (13.10 ft). Apogee: 300 km (180 mi).

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.



Family: orbital launch vehicle. Country: Japan. Engines: LE-5B engine, LE-7A. Stages: H-2A-1, H-2A LRB, LE-5B, SRB-A. Agency: Mitsubishi.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use