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
Gosling 4
Part of Gosling stage
RO solid rocket engine. Skylark 10A second stage, INTA-300 first stage.

AKA: INTA-300-1;Skylark 10A-2. Status: Retired 1974. Thrust: 137.00 kN (30,798 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 72 kg (158 lb). Burn time: 3.10 s. Height: 3.60 m (11.80 ft). Diameter: 0.26 m (0.85 ft).



Country: UK. Launch Vehicles: INTA-300, Skylark 10A, Fulmar, INTA-300B. Propellants: Solid. Stages: Gosling 4. 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