Martin T4M

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T4M/TG

Martin T4M

Type Torpedo bomber
Manufacturer Glenn L. Martin Company/Great Lakes Aircraft Company
Maiden flight 1927
Introduced 1928
Retired 1938
Primary user United States Navy
Number built 155
Developed from Martin T3M

The Martin T4M was a American torpedo bomber of the 1920s. A development by the Glenn L. Martin Company of their earlier Martin T3M, and like it a single engined biplane, the T4M served as the standard torpedo bomber aboard the aircraft carriers of the United States Navy through much of the 1930s.

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[edit] Development and design

The Martin Model 74 was designed and developed by the Glenn L. Martin Company as a result of testing of the experimental radial engined developments of the Martin T3M, the XT3M-3 and XT3M-4. The resulting prototype, designated XT4M-1, first flew in April 1927,[1] and was purchased by the U.S. Navy for further evaluation.[2]

The XT4M-1 had new single-bay fabric covered metal wings of shorter span than the wooden wings of the T3M.[3] It was powered by a Pratt & Whitney Hornet, (as used by the XT3M-3), and was fitted with a revised rudder. The fuselage was similar to that of the T3M-2, and like the earlier aircraft, could be fitted with either a wheeled undercarriage or floats.

As a result of the successful trials, the U.S. Navy ordered 102 similar production aircraft from Martin as the T4M-1 on June 30, 1927.[2] Martin sold their Cleveland factory, which had built the T4M, to the Great Lakes Aircraft Company in October 1928, which resulted in Great Lakes receiving an order for 18 aircraft with slightly modified undercarriages as the TG-1.[4] On July 2, 1930 the U.S. Navy placed an order for 32 aircraft powered by a more powerful Wright Cyclone radial engines with the Detroit Aircraft Corporation as the TE-1.[2] Detroit, however, passed the order to Great Lakes, which by this time was a subsidiary, and the aircraft were built as TG-2s.[2]

[edit] Operational history

T4M
T4M

Deliveries of the T4M to the U.S. Navy started in August 1928, replacing T3M-2s aboard the aircraft carriers USS Saratoga and Lexington.[4] Deliveries continued until 1931.[2]

While its predecessor, the T3M spent much of its time operating from floats, by the time the T4M and TG entered service, the U.S. Navy had realised the greater versatility of the aircraft carrier, and the T4Ms and TGs were mainly operated with wheeled undercarriages from the decks of carriers.[4] The capability of carrier based air power was demonstrated in fleet exercises in January 1929, when aircraft from the Saratoga, including T4Ms carried out mock attacks on the Panama Canal. Despite a defending force including the Lexington and shore based Navy and Army aircraft, the strike force was judged to have "destroyed" the canal locks as well as airfields. The exercise was described as "the most brilliantly conceived and most effectively executed naval operation in our history" by Admiral William V Pratt, who later became Commander in Chief of the U.S. Fleet.[5]

The T4M and TG proved difficult to replace, with both the XT6M and XT3D being evaluated but failing to demonstrate sufficient improvement to justify purchase.[6] They remained in service until 1938,[2] being eventually replaced by the TBD Devastator monoplane and becoming the last biplane torpedo bomber of the U.S. Navy.[7]

[edit] Variants

XT4M-1
Prototype. Powered by 525 hp (392 kW) Pratt & Whitney R-1690-24 engine. One built.
T4M-1
Initial production version by Martin, powered by R-1690-24 engine. 102 built.
TG-1
Version with slightly modified undercarriage, powered by 525 hp (392 kW) Pratt & Whitney R-1690-28 engine. 18 built by Great Lakes.
TG-1 Commercial
Civil version of TG-1. 2 built.[8]
TG-2
Version powered by 620 hp (463 kW) Wright R-1820-86 Cyclone. 32 built by Great Lakes (originally ordered as TE-1).

[edit] Operators

Flag of the United States United States

[edit] Specifications (T4M-1)

Data from United States Navy Aircraft since 1911 [7]

General characteristics

  • Crew: 3
  • Length: 35 ft 7 in (10.85 m)
  • Wingspan: 53 ft 0 in (16.16 m)
  • Height: 14 ft 9 in (4.50 m)
  • Wing area: 656 ft² (70.0 m²)
  • Empty weight: 5,814 lb (2,643 kg)
  • Loaded weight: 9,503 lb (4,320 kg)
  • Powerplant:Pratt & Whitney R-1690 Hornet 9 cylinder air-cooled radial engine, 525 hp (392 kW)

Performance

Armament

  • One flexibly mounted 0.3 in machine gun in rear cockpit
  • One torpedo or bombs under fuselage

[edit] See also

Related development

Comparable aircraft

Related lists

[edit] References

[edit] Notes

  1. ^ Swanborough and Bowers 1976, p.311
  2. ^ a b c d e f Grossnick 1995, p.508.
  3. ^ Taylor 1981, p.93.
  4. ^ a b c Swanborough and Bowers 1976, p.312
  5. ^ Polmar 2004, p41-43
  6. ^ Johnson 2005, p.4-5
  7. ^ a b Swanborough and Bowers 1976, p.313
  8. ^ Great Lakes Aerofiles. Retrieved 27 March 2008.
  9. ^ Johnson 1977, p.96
  10. ^ Johnson 1977, p.107.
  11. ^ Range carrying torpedo. When used in reconnaissance role, range "almost 700 mi" (610 NM, 1,100 km) - Polmar 2005, p.41

[edit] Bibliography

[edit] External links

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