Bristol M1 Monoplane

The Bristol M.1A Scout Monoplane was produced by Bristol Aeroplane Company as a private venture, flying for the first time at Filton on 14th July 1916.

 

Designed by Frank Barnwell, the type featured shoulder-mounted wire braced monoplane wings and a large domed prop spinner closely faired to the circular cowling of its 110 hp Clerget rotary engine. This was mounted at the front of a faired circular-section fuselage.

 

Barnwell had identified during the opening years of World War 1, that existing biplanes lacked performance. He specifically configured a circular cross-section fuselage, made of wooden and fabric construction, all designed for maximum speed.  Driven by a Clerget rotary engine with a twin-blade propeller, the Bristol M.1A could achieve a maximum speed of 132 mph, boasting a climb-rate at 10,00 ft in just 8 minutes 30 seconds.  The only real criticism made by the War Office Evaluation pilots was that it had poor forward and downward vision.

 

Four modified Bristol Type M.1B's were ordered with a pyramidical cabane structure and Vickers machine gun mounted in the port wing root although the design was rejected for use on the Western Front due to its landing speed which at 49mph was too fast for the majority of the French airfields.  Despite it being up to 50mph faster than any enemy aircraft in the sky at the time, many also considered it inherently unsafe in combat.

 

The Royal Flying Corps (RFC) imposed a ban on monoplanes after the crash of a Bristol Coanda monoplane,   and despite the 1913 Monoplane Committee clearing the type, the deep-rooted suspicion of single wing aeroplanes continued.

 

 

The production aircraft, of which 125 were ordered on 3rd August 1917, were the Bristol M.1C with a 110 hp Le Rhône engine, and the single forward-firing Vickers gun mounted on the centre-line. As a result of the lack of acceptance on the Western Front, the type was operationally based mainly overseas, flying operationally in the Balkans and Middle East and in use in countries such as Chile.

 

After the War, a number of Bristol M.1C were operated by private owners and one aircraft (VH-UQI / G-AUCH) continued flying until 1938, having been re-engined with a De Havilland Gipsy II engine.

 

The sole surviving Bristol M.1D Monoplane was a later, one-off conversion of a Bristol M.1C Monoplane, used for high speed testing of the Bristol Lucifer three cylinder radial engine.