AKA: Emma-0. Status: Retired 1963. Thrust: 14.80 kN (3,327 lbf). Gross mass: 20 kg (44 lb). Unfuelled mass: 13 kg (28 lb). Burn time: 1.00 s. Height: 0.80 m (2.62 ft). Diameter: 0.13 m (0.42 ft).
Matra solid rocket engine. Emma zero stage.
Country: France. Launch Vehicles: Emma. Propellants: Solid. Stages: SEPR P191. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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