The Wayback Machine - https://web.archive.org/web/20161228014703/http://astronautix.com/r/raven8.html
Raven 8

Encyclopedia Astronautica
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

Raven 8
Part of Rook engine Family
RO solid rocket engine. Skylark 4 second stage.

AKA: Skylark 4-2. Status: Retired 1989. Thrust: 50.10 kN (11,263 lbf). Gross mass: 1,100 kg (2,400 lb). Unfuelled mass: 230 kg (500 lb). Burn time: 30 s. Height: 5.40 m (17.70 ft). Diameter: 0.44 m (1.44 ft).

Country: UK. Launch Vehicles: Skylark 2, Skylark 2 AC, Skylark 4, Skylark 4 AC. Propellants: Solid. Stages: Raven 8. Agency: RO.



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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use