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H-2A SRB-A
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Gross Mass: 76,400 kg (168,400 lb). Empty Mass: 10,400 kg (22,900 lb). Thrust (vac): 2,250.000 kN (505,820 lbf). Isp: 280 sec. Burn time: 101 sec. Propellants: Solid. Propellant Formulation: HTPB. Isp(sl): 230 sec. Diameter: 2.50 m (8.20 ft). Span: 2.50 m (8.20 ft). Length: 15.20 m (49.80 ft). Country: Japan. No Engines: 1. Engine: SRB-A. Status: In production. First Flight: 2001. Last Flight: 2006. No Launched: 20. No Failed: 1. Shorter monolithic motor using filament-wound case technology from Thiokol. Version for J-1 has 1,000 kg less propellant and 1,200 kg less empty mass.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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