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H-IIA 2024
Part of H-2 Family
Japanese orbital launch vehicle. Three stage vehicle consisting of 4 x Castor 4XL + 2 x H-II SRB-A boosters + two-stage core vehicle.

Status: Active. First Launch: 2002-02-04. Last Launch: 2008-02-23. Number: 7 . Payload: 11,730 kg (25,860 lb). Thrust: 4,680.00 kN (1,052,100 lbf). Gross mass: 289,000 kg (637,000 lb). Height: 49.00 m (160.00 ft). Diameter: 4.00 m (13.10 ft). Apogee: 300 km (180 mi).

LEO Payload: 11,730 kg (25,860 lb) to a 300 km orbit at 30.40 degrees. Payload: 5,000 kg (11,000 lb) to a GTO. Development Cost $: 800.000 million. Launch Price $: 90.000 million in 1999 dollars in 1999 dollars.


More at: H-IIA 2024.

Family: orbital launch vehicle. Country: Japan. Engines: LE-5B engine, LE-7A. Spacecraft: DASH 2002, MDS, DRTS, USERS, IGS, DS2000, Kizuna. Launch Sites: Tanegashima, Tanegashima Y. Stages: Castor 4XL, H-2A-1, LE-5B, SRB-A. Agency: Mitsubishi.

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