Asp II engine (original) (raw)

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

Asp II engine

Cooper solid rocket engine. Asp III 4L first stage.

AKA: Asp II;Asp III 4L-1. Status: Retired 1959. Number: 1 . Thrust: 26.00 kN (5,845 lbf). Gross mass: 100 kg (220 lb). Unfuelled mass: 18 kg (39 lb). Burn time: 3.60 s. Height: 2.70 m (8.80 ft). Diameter: 0.17 m (0.54 ft).

Subtopics

RM-1100 Cooper solid rocket engine.

RM-1400 Cooper solid rocket engine.

Country: USA. Launch Vehicles: Asp III, Asp II. Propellants: Solid. Stages: Asp II engine. Agency: Cooper Development.

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