Tomahawk

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Model: Nike Tomahawk-2. Gross Mass: 200 kg (440 lb). Empty Mass: 60 kg (132 lb). Thrust (vac): 53.000 kN (11,914 lbf). Burn time: 9.50 sec. Propellants: Solid. Diameter: 0.22 m (0.72 ft). Length: 3.50 m (11.40 ft). Country: USA. No Engines: 1. Motor: TE-416. Status: Retired 1995. First Flight: 1963. Last Flight: 1995. No Launched: 538. Used as: Tomahawk. Release conditions: Thiokol. Used on Launch Vehicles: Strypi. Tomahawk Sandia. 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 - 2008 except where otherwise noted.