Fairey Stooge
| Stooge | |
|---|---|
Radio command |
The
Development
During
The British Army had already ordered early studies on these weapons.[4] According to a common account of its development, possibly apocryphal,[2] Fairey was asked to carry out some basic research on these plans by a Royal Navy request, but instead presented a revised design of some depth. The Ministry of Supply (MoS) signed a contract for development of the system in 1944. The ending of the war in August 1945 led to a lower level of urgency, but the MoS continued funding as a development project.[2]
Description
The Stooge was essentially a small subsonic aircraft with straight wings and a conventional tail layout. The missile looked substantially similar to the V-1, shrunken down and with the engine removed from the top. The missile fuselage was 7 ft 5.5 in (2.273 m) long and 12.5 in (320 mm) in diameter, with a main wingspan of 6 ft 10 in (2.08 m), and a tail span of 4 ft (1.2 m). Ready for launch, it weighed 738 lb (335 kg).[5]
The rear part of the fuselage was taken up by four 5-inch (130 mm) air-to-ground "Swallow"
For launch, four rocket motors (from the
Like many early missiles of the era, the Stooge was boosted to the approximate altitude of the attacker and then flown onto an intercept course. Flares located in fairings on the wing tips provided a bright source for the operator to track visually.[7] After launch the missile levelled off and a simple gyroscope-controlled autopilot, located in the forwards portion of the fuselage,[8] kept the Stooge flying in a straight line. Control of first the elevators and then, 3 seconds later, the ailerons were released to the operator - the delay necessary for the gyro control to stabilise first. Using radio control, the operator would fly the missile into a position in front of the target, and then adjust the path in order to collide with the target. Control was via the ailerons and elevator, the vertical stabilizer did not contain a movable rudder.[7]
Flight testing
The first prototypes, with fixed controls, flew after seven months from the start of development at the end of World War II.[6] Development continued with a number of test firings at the Rocket Experimental Establishment at RAF Aberporth at Aberporth, Wales.[8] It is believed that around twelve Stooges were constructed by Fairey, the most successful of the test launches being that of the sixth missile, achieving an altitude of 1,600 feet (490 m) and a range of 3 miles (4.8 km) before the flight was terminated by range safety, the missile having passed out of sight of the operator.[9]
The Stooge, on its launcher, was displayed at the Radlett Aerodrome in 1947.[10] Radlett, northwest of London, was the site of a major Handley Page factory and host of early meetings of what would become the Farnborough Airshow.
Although the programme failed to yield an operational weapons system, experience gained from the testing of Stooge assisted in the development of the
See also
- Brakemine, another early UK missile using beam riding guidance rather than radio control
References
- Citations
- ^ Ford 2000, p.101
- ^ a b c Taylor 1975, p.45
- ^ Parsch 2003
- ^ Flight 1947, p.345
- ^ a b c Flight 1947, p.344
- ^ a b c Taylor 1974, p.46
- ^ a b c d Flight 1947, p.344-345
- ^ a b c Taylor 1974, p.47
- ^ Taylor 1974, p.48
- ^ "The Stooge at Radlett" Archived 10 June 2015 at the Wayback Machine, Flight, 11 September 1947, p. 271.
- ^ Twigge 1993, p.24
- Bibliography
- "Fairey's First Guided Missile", Flight, 17 April 1947, pp. 344–345
- Ford, Roger (2000). Germany's Secret Weapons in World War II. Osceola, WI: MBI Publishing. p. 101. ISBN 0-7603-0847-0. Retrieved 22 October 2011.
- Parsch, Andreas (2003). "SAM-N-2/SAM-N-4". Directory of U.S. Military Rockets and Missiles, Appendix 1: Early Missiles and Drones. designation-systems.net. Retrieved 22 October 2011.
- Taylor, H.A. (1974). Fairey Aircraft since 1915 (1988 reprint ed.). Annapolis, MD: Naval Institute Press. ISBN 0-87021-208-7. Retrieved 22 October 2011.
- Twigge, Stephen Robert (1993). The Early Development of Guided Weapons in the United Kingdom, 1940-1960. Chur, Switzerland: Harwood Academic Publishers. ISBN 3-7186-5297-8. Retrieved 22 October 2011.