| Designed by R F Mann and R P Grimmer, the M.I twoseat
fighter represented an attempt to combine the
superior performance offered by a tractor configuration
with the clear forward field of fire provided by a pusher
arrangement. The conventionally-mounted Anzani 10-
cylinder air-cooled radial engine drove two pusher propellers
by means of an extended shaft via a gearbox
and chains. The gunner was seated immediately aft of
the engine, the pilot's cockpit being just behind the
plane of the propellers. The M.1 was first flown on 19
February 1915, but difficulties were experienced with
the chain transmission and with handling. Various
modifications were made and the 100hp Anzani engine
was replaced by one rated at 125hp, but after some 18 hours of flight testing, the M.1 was wrecked on 16
November 1915 before it could be evaluated by the RFC,
and although work on the prototype of an improved version,
the M.2, was begun, no further aircraft was completed.
| A three-view drawing (1278 x 820) |
WEIGHTS |
Take-off weight | 1270 kg | 2800 lb |
Empty weight | 953 kg | 2101 lb |
DIMENSIONS |
Wingspan | 10.59 m | 35 ft 9 in |
Length | 8.05 m | 26 ft 5 in |
Wing area | 29.91 m2 | 321.95 sq ft |
PERFORMANCE |
Max. speed | 137 km/h | 85 mph |
L B Mann, e-mail, 03.12.2010 20:07 Do you have any information about R F Mann? We may be related.
Thank you. reply |
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| All the World's Rotorcraft |