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
RM-1400
Part of Asp II engine Family
Cooper solid rocket engine.

AKA: Asp IV. Status: Retired 1963. Thrust: 12.70 kN (2,855 lbf). Gross mass: 94 kg (207 lb). Unfuelled mass: 27 kg (59 lb). Burn time: 12 s. Height: 2.80 m (9.10 ft). Diameter: 0.17 m (0.54 ft).



Country: USA. Launch Vehicles: Nike Asp, Asp IV, Terrier Asp IV. Propellants: Solid. Stages: RM-1400. 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use