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Algol 3


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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 3 Part of Algol CSD solid rocket engine. Used on Advanced Scout, Scout D, Scout F, Scout G. First flight 1972.

Status: First flight 1972. Number: 36 . Thrust: 471.90 kN (106,087 lbf). Gross mass: 14,320 kg (31,570 lb). Unfuelled mass: 1,600 kg (3,500 lb). Specific impulse: 284 s. Specific impulse sea level: 238 s. Burn time: 75 s. Height: 9.40 m (30.80 ft). Diameter: 1.14 m (3.74 ft).

Thrust (sl): 395.500 kN (88,912 lbf). Thrust (sl): 40,327 kgf.

Country: USA. Launch Vehicles: Scout D-1, Scout F-1, Scout G-1, Scout D, Advanced Scout. Propellants: Solid. Stages: Algol 3. 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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