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S400
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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 S400 Liquid propellant rocket engines manufactured by Airbus, used primarily as apogee engines for telecommunications satellites. The chamber and throat are made of platinum alloy, using a double cone vortex injector and both film and radiative cooling.
Thrust: 96 N (21 lbf). Gross mass: 4.30 kg (9.40 lb). Specific impulse: 321 s. Height: 0.67 m (2.19 ft). Diameter: 0.32 m (1.04 ft).
Country: France. Propellants: MON/MMH. Agency: Airbus. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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