Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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 1A
Part of Antares Family
Thiokol solid rocket engine. Used on Blue Scout 1, Blue Scout 2, Blue Scout Junior, Scout X-1. First flight 1960.

AKA: Star 31;X-254. Status: Retired 1970. Number: 45 . Thrust: 60.50 kN (13,601 lbf). Gross mass: 1,225 kg (2,700 lb). Unfuelled mass: 294 kg (648 lb). Specific impulse: 256 s. Specific impulse sea level: 233 s. Burn time: 39 s. Height: 3.38 m (11.08 ft). Diameter: 0.78 m (2.55 ft).

Thrust (sl): 55.100 kN (12,387 lbf). Thrust (sl): 5,615 kgf.



Country: USA. Launch Vehicles: WASP, Scout X, Scout X-1, Blue Scout Jr, Blue Scout Junior, Blue Scout I, Blue Scout II, Scout X-1A, Blue Scout Jr SLV-1C, RAM B, Blue Scout Jr SLV-1B(m). Propellants: Solid. Stages: Antares 1A. Agency: Thiokol.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use