SEPR P191

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Engine Model: SEPR P191. Designer: Matra. Gross Mass: 20 kg (44 lb). Empty Mass: 13 kg (28 lb). Propellants: Solid. Thrust(vac): 14.800 kN (3,327 lbf). Burn time: 1.00 sec. Diameter: 0.13 m (0.42 ft). Length: 0.80 m (2.62 ft). Country: France. SEPR P191 used on Rocket Stages Used on stage: Emma. on launch vehicle: Emma. 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.