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Ajax engine


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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 Ajax engine Part of Ajax Bell liquid rocket engine for the Nike Ajax sustainer stage. Red fuming nitric acid was the oxidizer; in the test missiles, the fuel was aniline-furfuryl alcohol as fuel, changing to JP-4 kerosene in the production missiles. Nike Ajax second stage.

AKA: Ajax;Nike Ajax-2. Status: Retired 1963. Thrust: 11.60 kN (2,608 lbf). Gross mass: 200 kg (440 lb). Unfuelled mass: 372 kg (820 lb). Burn time: 71 s. Height: 4.50 m (14.70 ft). Diameter: 0.30 m (0.98 ft).

Country: USA. Engines: Ajax engine. Launch Vehicles: Nike Ajax. Propellants: Solid. Agency: Bell. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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