Castor 2 Gross Mass: 4,424 kg (9,753 lb). Empty Mass: 695 kg (1,532 lb). Thrust (vac): 258.915 kN (58,206 lbf). Isp: 262 sec. Burn time: 37 sec. Propellants: Solid. Isp(sl): 232 sec. Diameter: 0.79 m (2.59 ft). Span: 0.79 m (2.59 ft). Length: 6.04 m (19.81 ft). Country: USA. No Engines: 1. Engine: TX-354-3. Cost $ : 1.010 million. First Flight: 1960. Last Flight: 1994. No Launched: 1054. Used as: Scout A; Delta E. Used on Launch Vehicles: Advanced Scout. Blue Scout 1. Blue Scout 2. Blue Scout Junior. Delta 0100. Delta 1000. Delta 2000. Delta E. Delta J. Delta L. Delta M. Delta N. H-1. N. N-2. Scout A. Scout B. Scout D. Scout F. Scout G.                   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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