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SICBM-1


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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 SICBM-1 Part of Castor 4 Thiokol solid rocket engine.

AKA: SICBM. Status: Retired 1991. Number: 1 . Thrust: 979.00 kN (220,087 lbf). Gross mass: 11,600 kg (25,500 lb). Burn time: 40 s. Height: 7.50 m (24.60 ft). Diameter: 1.17 m (3.83 ft).

Country: USA. Launch Vehicles: SICBM. Propellants: Solid. Stages: SICBM-1. 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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