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
Snipe
RO solid rocket engine. Fulmar second stage.

AKA: Fulmar-2. Status: Retired 1994. Thrust: 16.00 kN (3,596 lbf). Gross mass: 200 kg (440 lb). Unfuelled mass: 58 kg (127 lb). Burn time: 16 s. Height: 2.10 m (6.80 ft). Diameter: 0.26 m (0.85 ft).

Country: UK. Launch Vehicles: INTA-300, Fulmar, INTA-300B. Propellants: Solid. Stages: Snipe. Agency: RO.
Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use