H-1-0 Gross Mass: 4,480 kg (9,870 lb). Empty Mass: 750 kg (1,650 lb). Thrust (vac): 258.915 kN (58,206 lbf). Isp: 265 sec. Burn time: 39 sec. Propellants: Solid. Isp(sl): 235 sec. Diameter: 0.79 m (2.59 ft). Span: 0.79 m (2.59 ft). Length: 6.04 m (19.81 ft). Country: Japan. No Engines: 1. Engine: TX-354-3. Status: In Production. Cost $ : 2.000 million. Other designations: License built Castor II.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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