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H-IIA 202
Part of H-2 Family
Japanese orbital launch vehicle. Three stage version of H-IIA consisting of 2 x H-II SRB-A + two-stage core vehicle.

Status: Active. First Launch: 2001-08-29. Last Launch: 2017-03-17. Number: 19 . Payload: 10,000 kg (22,000 lb). Thrust: 5,600.00 kN (1,258,900 lbf). Gross mass: 285,000 kg (628,000 lb). Height: 53.00 m (173.00 ft). Diameter: 4.00 m (13.10 ft). Apogee: 40,000 km (24,000 mi).

LEO Payload: 10,000 kg (22,000 lb). Payload: 4,100 kg (9,000 lb) to a GTO.


More at: H-IIA 202.

Family: orbital launch vehicle. Country: Japan. Spacecraft: Daichi-2, Akatsuki, DCAM, DESPATCH, Ginrei, GPM, Horyu, Ikaros, MASCOT, Minerva II, Raijin, Shin'en, Shizuku, SOCRATES, SPROUT, STARS-2, Target Marker, Teikyosat, UNIFORM, Unitec, VEP, ADEOS, KOMPSAT, LRE, FedSat, Mu-Labsat, WEOS Kanta-Kun, IGS, Hayabusa, Cubesat, DS2000, Ibuki, JAXA SDS, Kagayaki, KKS, Kukai, PRISM, SOHLA, SpriteSat. Launch Sites: Tanegashima, Tanegashima Y. Stages: H-2A-1, LE-5B, SRB-A. Agency: Mitsubishi.

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