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M a r t i n M O
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A p p e a r a n c e
F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
In the early 1920s the United States Navy became interested in a thick airfoil section, cantilever wing, United States military observation aircraft, developed by the Dutch company Fokker . The Navy's Bureau of Aeronautics designed a three-seat observation monoplane to use a similar wing. Production of the aircraft, designated the MO-1 , was contracted to the Glenn L. Martin Company with an order for 36 aircraft. The MO-1 was a shoulder-wing cantilever monoplane with a slab-sided fuselage and a fixed tailwheel landing gear. It had an all-metal structure with a fabric covering, and was powered by a Curtiss D-12 engine. In 1924 one aircraft was fitted with float landing gear for evaluation.
Variants
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MO-1
Production version for the United States Navy, 36 built.
Operators
[ edit ]
United States
[ edit ]
Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2419
General characteristics
Crew: three
Wingspan: 53 ft 1 in (16.18 m )
Powerplant: 1 × Curtiss D-12 , 435 hp (324 kW)
Performance
Maximum speed: 105 mph (169 km/h, 91 kn )
Related lists
References
[ edit ]
John Andrade, U.S.Military Aircraft Designations and Serials since 1909, Midland Counties Publications, 1979, ISBN 0-904597-22-9 (Page 204)
The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2419
External links
[ edit ]
Martin MO at Wikimedia Commons
t
e
Model numbers
Airliners
Attack aircraft
Bombers
Maritime patrol
Military transports
Military trainers
Scout/Torpedo bombers
Reconnaissance aircraft
Observation aircraft
Martin Marietta
t
e
USN observation aircraft designations, pre-1962
Observation
Observation Scout
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United States
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