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Contents

   



(Top)
 


1 Design and development  





2 Operational history  





3 Specifications  





4 See also  





5 References  



5.1  Notes  





5.2  Bibliography  
















Lockheed Big Dipper






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From Wikipedia, the free encyclopedia
 


Model 34 Big Dipper
Role Two-seat utility monoplane
National origin United States
Manufacturer Lockheed
Designer John Thorp
First flight 10 December 1945
Status Crashed 6 February 1946
Number built 1

The Lockheed Model 34 Big Dipper was an American two-seat monoplane, designed and built by LockheedatBurbank for research into the company's potential entry into the civil lightplane and military light utility aircraft market. Only one was built, and following its loss in an accident the program was abandoned.

Design and development[edit]

Developed by John Thorp and based on his work on Lockheed's Little Dipper lightplane project,[1] the Lockheed Model 34, named "Big Dipper", was intended as a prototype for a lightplane to sell on the postwar market - Lockheed hoping to sell the aircraft at a price of $1500[2] - and as a potential 'flying jeep' for the United States Army.[1] It was a low-wing cantilever monoplane with a fixed tricycle landing gear and a conventional empennage; the cabin was enclosed, seating two in side-by-side positions. Unusually the Continental C100 piston engine was fitted in the center fuselage behind the cabin, driving a two-bladed pusher propeller mounted at the rear of the aircraft.[2]

Operational history[edit]

The Model 34 was built at Burbank from July 1945. To keep the project secret the aircraft was moved to Palmdale by road when completed, flight testing being conducted at Muroc Dry Lake.[2] It first flew on 10 December 1945, and after 40 hours of flight testing was returned to Burbank for modifications,[3] intended to correct a wing-root stall issue that had been identified.[4] It was decided not to complete the modification, and the aircraft was to be flown back to Palmdale on 6 February 1946. To try to keep the Big Dipper secret, it was decided to use a shorter upward sloping runway nearer the factory; in the steep climb needed during takeoff from the shorter runway, the aircraft stalled and crashed.[3] With the loss of the prototype, and the fact the expected rush of buyers for new lightplanes was failing to materialize amidst a glut of war-surplus aircraft,[5] the project, and a proposed high-wing four-seat "Super Dipper" derivative, was abandoned;[3]

Specifications[edit]

Cockpit of the Big Dipper

Data from Francillon 1982[3]

General characteristics

Performance

See also[edit]

Related development

Aircraft of comparable role, configuration, and era

References[edit]

Notes[edit]

  1. ^ a b Francillon 1982, pp. 277
  • ^ a b c Walker, Franklin D. (March 1946). "Report From Washington". Flying. Vol. 38, no. 3. Chicago: Ziff-Davis Publishing. p. 43.
  • ^ a b c d Francillon 1982, pp. 278-279
  • ^ Badrocke and Gunston 1998, p. 37.
  • ^ Westwick 2012, p. 66.
  • Bibliography[edit]

  • Francillon, René J. (1982). Lockheed Aircraft since 1913. London: Putnam & Company. ISBN 0-370-30329-6.
  • Westwick, Peter J. (2012). Blue Sky Metropolis: The Aerospace Century in Southern California. Berkeley, CA: University of California Press. ISBN 978-0-520-28906-2.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Lockheed_Big_Dipper&oldid=1063280187"

    Categories: 
    Lockheed aircraft
    1940s United States civil utility aircraft
    Single-engined pusher aircraft
    Mid-engined aircraft
    Low-wing aircraft
    Aircraft first flown in 1945
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Commons category link is on Wikidata
     



    This page was last edited on 2 January 2022, at 04:13 (UTC).

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