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Algol 3A


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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 Algol 3A Part of Algol CSD solid rocket engine. In Production.

Status: In Production. Thrust: 464.70 kN (104,469 lbf). Gross mass: 14,732 kg (32,478 lb). Unfuelled mass: 2,030 kg (4,470 lb). Specific impulse: 259 s. Specific impulse sea level: 226 s. Burn time: 84 s. Height: 9.40 m (30.80 ft). Diameter: 1.14 m (3.74 ft).

Thrust (sl): 405.500 kN (91,160 lbf). Thrust (sl): 41,349 kgf. Chamber Pressure: 31.00 bar. Area Ratio: 6.5.

Country: USA. Launch Vehicles: Scout D-1 F, Scout E-1. Propellants: Solid. Stages: Algol 3A. Agency: CSD. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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