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Antares 2


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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 Antares 2 Part of Antares Thiokol solid rocket engine. Used on Scout A, Scout B, Scout D, Scout F, Scout X-2, Scout X-3, Scout X-4. First flight 1962.

AKA: X-259. Status: Retired 1995. Number: 92 . Thrust: 93.10 kN (20,930 lbf). Gross mass: 1,400 kg (3,000 lb). Unfuelled mass: 300 kg (660 lb). Specific impulse: 293 s. Specific impulse sea level: 233 s. Burn time: 36 s. Height: 2.90 m (9.50 ft). Diameter: 0.78 m (2.55 ft).

Thrust (sl): 74.000 kN (16,635 lbf). Thrust (sl): 7,549 kgf.

Country: USA. Launch Vehicles: Scout A, Scout X-2, Scout X-2M, Scout X-3A, Scout X-3, Scout X-2 1C, Scout X-3M, Scout X-4, Scout X-2B, Scout X-4A, Scout X-3C, Scout B, Scout B 2A, SPARTA, Scout X-5C, Athena H, Scout B-1, Scout B-1 F, Scout D-1, Scout D-1 F, Scout A-1, Scout E-1, Scout F-1, Scout D, Strypi XI, Strypi IX, Strypi Tomahawk. Propellants: Solid. Stages: Antares 2. Agency: Thiokol. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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