HTR

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Model: Hybrid Test Rocket-1. Gross Mass: 500 kg (1,100 lb). Thrust (vac): 30.000 kN (6,744 lbf). Burn time: 20 sec. Propellants: Lox/Solid. Diameter: 0.25 m (0.82 ft). Length: 10.00 m (32.00 ft). Country: USA. No Engines: 1. Motor: HTR. Status: Active. Used as: HTR. Release conditions: Nammo. Used on Launch Vehicles: Hybrid Test Rocket. 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.