P6

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Model: Veronique P6-1. Gross Mass: 500 kg (1,100 lb). Thrust (vac): 20.000 kN (4,496 lbf). Propellants: Solid. Diameter: 0.55 m (1.80 ft). Length: 6.00 m (19.60 ft). Country: France. No Engines: 1. Motor: Vero P6. Status: Retired 1952. First Flight: 1952. Last Flight: 1952. No Launched: 2. Used as: Veronique. Release conditions: LRBA. Model: Diamant-3. Gross Mass: 703 kg (1,549 lb). Empty Mass: 68 kg (149 lb). Thrust (vac): 29.400 kN (6,609 lbf). Isp: 211 sec. Burn time: 39 sec. Propellants: Solid. Isp(sl): 211 sec. Diameter: 0.66 m (2.16 ft). Span: 0.66 m (2.16 ft). Length: 1.98 m (6.49 ft). Country: France. No Engines: 1. Motor: P6. Status: Out of production. Cost $ : 3.000 million. First Flight: 1964. Last Flight: 1972. No Launched: 16. No Failed: 1. Other designations: P-6. Model: Diamant B-3. Gross Mass: 800 kg (1,760 lb). Empty Mass: 120 kg (260 lb). Thrust (vac): 50.000 kN (11,240 lbf). Isp: 211 sec. Burn time: 46 sec. Propellants: Solid. Isp(sl): 211 sec. Diameter: 0.80 m (2.62 ft). Span: 0.80 m (2.62 ft). Length: 1.67 m (5.47 ft). Country: France. No Engines: 1. Motor: P6. Status: Out of production. Cost $ : 4.000 million. First Flight: 1970. Last Flight: 1975. No Launched: 12. Other designations: P-6. Used on Launch Vehicles: Berenice. Diamant. Europa. Veronique. 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.