FFAR

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Engine Model: FFAR. Empty Mass: 5.00 kg (11.00 lb). Propellants: Solid. Thrust(vac): 3.600 kN (809 lbf). Burn time: 1.50 sec. Diameter: 0.0700 m (0.2290 ft). Length: 1.20 m (3.90 ft). Country: USA. FFAR used on Rocket Stages Used on stage: FFAR. on launch vehicle: FFAR. Used on stage: FFAR. on launch vehicle: HVAR. Used on stage: FFAR. on launch vehicle: Rockair. 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.