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
Goose II
RO solid rocket engine. INTA-255 first stage.

AKA: INTA-255-1. Status: Retired 1970. Thrust: 22.00 kN (4,945 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 95 kg (209 lb). Burn time: 17 s. Height: 3.40 m (11.10 ft). Diameter: 0.26 m (0.85 ft).

Country: UK. Launch Vehicles: INTA-255. Propellants: Solid. Stages: Goose II. 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