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词条 Martin MO
释义

  1. Variants

  2. Operators

  3. Specifications (MO-1)

  4. References

  5. External links

name=Martin MOimage=EL-2002-00565.jpgcaption=Martin MO-1 at Langley

}}{{Infobox Aircraft Type

type=Observation monoplanemanufacturer=Martindesigner=first flight= 14 December 1924introduced=retired=status=primary user=United States Navymore users=produced=number built=36variants with their own articles=
}}

The Martin MO was an American observation monoplane built by the Glenn L. Martin Company of Cleveland, Ohio for the United States Navy.

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

MO-1

Production version for the United States Navy, 36 built.

Operators

{{USA}}
  • United States Navy

Specifications (MO-1)

{{aerospecs
|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2419
|met or eng?=eng
|crew=three
|capacity=
|length m=
|length ft=
|length in=
|span m=16.18
|span ft=53
|span in=1
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=
|height ft=
|height in=
|wing area sqm=
|wing area sqft=
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=
|empty weight lb=
|gross weight kg=
|gross weight lb=
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=Curtiss D-12
|eng1 kw=324
|eng1 hp=435
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=169
|max speed mph=105
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|sequence=
|lists=
  • List of military aircraft of the United States (naval)

}}

References

  • 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

{{commons category-inline|Martin MO}}{{Martin aircraft}}{{USN observation aircraft}}

4 : United States military reconnaissance aircraft 1920–1929|Shoulder-wing aircraft|Single-engined tractor aircraft|Aircraft first flown in 1924

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