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H-2A SSB
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Gross Mass: 15,200 kg (33,500 lb). Empty Mass: 2,100 kg (4,600 lb). Thrust (vac): 626.600 kN (140,865 lbf). Isp: 283 sec. Burn time: 60 sec. Propellants: Solid. Propellant Formulation: HTPB. Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft). Length: 14.90 m (48.80 ft). Country: Japan. No Engines: 1. Engine: Castor 4AXL. Status: In production. First Flight: 2001. Last Flight: 2006. No Launched: 40. Provides supplemental thrust for H-2 or H-2A.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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