HTR

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Engine Model: HTR. Designer: Nammo. Propellants: Lox/Solid. Thrust(vac): 30.000 kN (6,744 lbf). Burn time: 20 sec. Country: USA. HTR used on Rocket Stages Used on stage: HTR. on launch vehicle: 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.