Miles Master
Template:Infobox Aircraft The Miles M.9 Master was a British 2-seat monoplane advanced trainer built by Miles Aircraft Ltd for the Royal Air Force and Fleet Air Arm during the Second World War. It went through a number of variants according to engine availability and was even modified as an emergency fighter during the Battle of Britain. It was a fast, strong and fully aerobatic aircraft and served as an excellent introduction to the high performance British fighter aircraft of the day; the Spitfire and Hurricane.
Design and development
The M.9A Master I was based on the M.9 Kestrel trainer that was first demonstrated at the Hendon Airshow in July 1937, although it never entered production. The M.9 Kestrel, powered by the 745 hp (555 kW) Rolls-Royce Kestrel XVI V-12 engine, could reach 295 mph (475 km/h). The production Master I, which first flew on 31 March, 1939, used the lower powered 715 hp (535 kW) Rolls-Royce Kestrel XXX engine, reducing the maximum speed. Nonetheless it remained one of the fastest and most maneuverable trainers of its day. The Master entered service just before the start of the war, and eventually 900 Mk. I and Mk. IA Masters were built. This total included 26 built as the M.24 Master Fighter which were modified to a single-seat configuration, and armed with six .303 in machine guns.
When production of the Kestrel engine ceased, a new variant of the Master was designed to use the 870 hp (650 kW) air-cooled radial Bristol Mercury XX engine. The first M.19 Master II prototype flew on 30 October, 1939 and 1,748 were eventually built. When the Lend-Lease programme began to supply engines from the United States, a third variant of the Master, the M.27 Master III was designed, powered by the American 825 hp (615 kW) Pratt & Whitney Twin Wasp Junior two-row radial engine. A total of 602 Master IIIs were built before production of the Miles Martinet took over in 1942.
In trainer form, the Master was equipped to carry eight practice bombs, plus one .303 in Vickers machine gun mounted in the front fuselage. In 1942, all variants had their wings clipped by three feet (one metre) to reduce stress on the wings and increase maneuverability.
Production
All the 3,227 Masters produced were built by Phillips and Powis Aircraft Limited at Woodley, Berkshire, the largest number produced of any Miles aircraft type.
Operational history
Service use primarily revolved around (Pilot) Advanced Flying Units, while several hundred Miles Master IIs were converted, or delivered new, for the glider-towing role, with the bottom of the rudder cut away to allow fitting of a towing hook. Miles Masters were extensively used from 1942 as tugs for Hotspur gliders at Glider Training Schools. Diversions from RAF stocks included 426 to the South African Air Force, 52 to the Fleet Air Arm, nine to the USAAF in rgw UK, 23 to the Royal Egyptian Air Force and, early in 1945, 23 to Turkey. Eleven also went to the Irish Air Corps and two to Portugal.
Military operators
Specifications (Mk II)
General characteristics
- Crew: Two (instructor and student)
- Airfoil: NACA 230
- Clipped wingspan: 35 ft 9 in (10.9 m)
- Wing area: 224 ft² (20.8 m²)
Performance
Armament
- 1 × .303 in Vickers K machine-gun
References
Notes
Bibliography
- Amos, Peter. and Brown, Don Lambert. Miles Aircraft Since 1925, Volume 1. London: Putnam Aeronautical, 2000. ISBN 0-85177-787-0.
- Brown, Don Lambert. Miles Aircraft Since 1925. London: Putnam & Company Ltd., 1970. ISBN 0-37000-127-3.
- Jane, Fred T. Jane's All the World's Aircraft 1945/6. London: Sampson Low Marston, 1946. ISBN 0-7153-5109-6.
- Mondey, David. The Hamlyn Concise Guide to British Aircraft of World War II. London: Chancellor Press, 1994. ISBN 1-85152-668-4.
- Temple, Julian C. Wings Over Woodley - The Story of Miles Aircraft and the Adwest Group. Bourne End, Bucks, UK: Aston Publications, 1987. ISBN 0-946627-12-6.
External links
See also
Related development Miles Kestrel - Miles Martinet Aircraft of comparable role, configuration, and era North American Harvard Related lists