P6 Designer: SNPE. Gross Mass: 800 kg (1,760 lb). Empty Mass: 120 kg (260 lb). Propellants: Solid. Thrust(vac): 29.400 kN (6,609 lbf). Thrust(sl): 29.400 kN (6,609 lbf). Isp: 211 sec. Isp (sea level): 211 sec. Burn time: 45 sec. Diameter: 1.50 m (4.90 ft). Length: 2.07 m (6.79 ft). Chambers: 1. Country: France. Status: Out of production. First Flight: 1965. Last Flight: 1973. Flown: 9.00. P6 used on Rocket Stages Used on stage: Diamant B-3. on launch vehicle: Diamant B. Used on stage: Diamant-3. on launch vehicle: Diamant A.                   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 - 2007 except where otherwise noted.

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