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H-IIA
Part of H-2

H-2 Cutaway view

H-2 Cutaway view
Credit: NASDA

Japanese orbital launch vehicle. Low-cost version of H-2 developed for the commercial market. The two SRB-A solid rocket boosters can be supplemented by 4 smaller SSB solid boosters. 0 or 2 SSB's can be fitted for reduced 9,940 kg or 10,740 kg LEO payloads.

AKA: H-2A;H-IIA 2024. Status: Active. First Launch: 2014-10-07. Last Launch: 2014-10-07. Number: 1 . 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.

Stage Data - H-2A



Family: orbital launch vehicle. Country: Japan. Spacecraft: HTV, VEP, LRE, DASH 2002, MDS, USERS, IGS, DS2000. Stages: SRB-A. Agency: Mitsubishi.

2014 October 7 - . 05:16 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA.

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