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SEPR P163


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z SEPR P163 Part of Emma Matra solid rocket engine. Emma first stage.

AKA: Emma-1. Status: Retired 1963. Thrust: 1.40 kN (315 lbf). Gross mass: 50 kg (110 lb). Unfuelled mass: 11 kg (24 lb). Burn time: 37 s. Height: 1.70 m (5.50 ft). Diameter: 0.13 m (0.42 ft).

Country: France. Launch Vehicles: Emma. Propellants: Solid. Stages: SEPR P163. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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