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Contents

   



(Top)
 


1 Design and development  





2 Operational history  





3 Specifications (Vultee XA-41)  





4 Notes  





5 Bibliography  





6 External links  














Vultee XA-41






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From Wikipedia, the free encyclopedia
 

(Redirected from Vultee 90)

XA-41
Vultee XA-41 during USAF testing (USAF photo)
Role Ground attack
National origin United States
Manufacturer Vultee Aircraft
First flight 11 February 1944 (Model 90)
Retired 1950
Status Experimental
Primary users United States Army Air Forces
United States Navy
Number built 1

The Vultee XA-41 was originally ordered as a dive bomber. After combat experience led the Army Air Corps to believe dive-bombers were too vulnerable to enemy fighters, the contract was amended to change the role to low-level ground attack. Although the XA-41 was a potent weapons system, the design was overtaken by more advanced technology, and never entered production.

Design and development

[edit]

The Vultee engineering team decided early in the design process to build the XA-41 (company Model 90) around the 3,000 hpPratt & Whitney R-4360 Wasp Major four-row, 28-cylinder radial engine. The Model 90's large tapered wing resembled that of Vultee Model 72 – a two-seat attack aircraft/dive bomber better known as the Vultee Vengeance (A-31/A-35) – including a straight leading edge, forward-swept trailing edge, and pronounced dihedral on the outer wing panels.

Designed to carry both a large internal load and external stores, the XA-41 was large for a single-engine aircraft. The single-place cockpit, set in line with the wing root, was 15 ft (4.6 m) off the ground when the airplane was parked.

As operational priorities shifted during its development phase, the original order for two XA-41 prototypes was cancelled, although the USAAF pressed for the completion of one prototype as an engine testbed for the R-4360 (the same engine used by the Boeing B-50 Superfortress).

Operational history

[edit]

Flying for the first time on 11 February 1944, the sole XA-41 (S/N 43-35124) proved to have good performance with a maximum speed of 354 mph reached in testing and "superb maneuverability, being able to out-turn a P-51B Mustang".[1] However, with the reduction in military orders due to the approaching end of the war, no production contract was placed, and the aircraft was used as an engine testbed for the USAAF as well as being evaluated by the U.S. Navy in comparison with other contemporary attack aircraft, especially the Douglas AD-1 Skyraider and Martin AM-1 Mauler. After its Navy trials, the XA-41, bearing civil registration NX60373N, was consigned to the Pratt & Whitney division of United Aircraft to continue engine tests. These continued until 1950 before the XA-41 was scrapped.

Specifications (Vultee XA-41)

[edit]
3-view line drawing of the Vultee XA-41
3-view line drawing of the Vultee XA-41

Data from Jane's all the World's Aircraft 1947[2]

General characteristics

Performance

Armament

plus

Notes

[edit]
  1. ^ Thompson 1992, p. 119.
  • ^ Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. pp. 205c–206c.
  • Bibliography

    [edit]
    [edit]
    Retrieved from "https://en.wikipedia.org/w/index.php?title=Vultee_XA-41&oldid=1147905823"

    Categories: 
    1940s United States attack aircraft
    Vultee aircraft
    Single-engined tractor aircraft
    Aircraft first flown in 1944
    Mid-wing aircraft
    Cancelled military aircraft projects of the United States
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Short description is different from Wikidata
    Aircraft specs templates using more performance parameter
    Commons category link is on Wikidata
     



    This page was last edited on 2 April 2023, at 23:02 (UTC).

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