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Contents

   



(Top)
 


1 Applications  





2 Specifications (Ounce)  



2.1  General characteristics  





2.2  Components  





2.3  Performance  







3 See also  





4 References  



4.1  Notes  





4.2  Bibliography  







5 External links  














Armstrong Siddeley Ounce






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From Wikipedia, the free encyclopedia
 


Ounce
Type Piston engine
National origin United Kingdom
Manufacturer Armstrong Siddeley
First run 1920

The Armstrong Siddeley Ounce was a small two-cylinder aero engine developed by Armstrong Siddeley in 1920.[1] The engine was originally conceived as a test piece but ran very well and was put into production for early ultralight aircraft and use in target drones. The Ounce used two cylinders from the preceding Jaguar I radial engine.

Applications[edit]

Specifications (Ounce)[edit]

Data from Lumsden.[2]

General characteristics

Components

Performance

See also[edit]

Comparable engines

Related lists

References[edit]

Notes[edit]

  1. ^ Gunston 1989, p.18.
  • ^ Lumsden 2003, p.66.
  • Bibliography[edit]

    • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.
  • External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Armstrong_Siddeley_Ounce&oldid=1102333791"

    Categories: 
    Armstrong Siddeley aircraft engines
    1920s aircraft piston engines
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Use dmy dates from August 2017
    Use British English from August 2017
    Commons category link is on Wikidata
     



    This page was last edited on 4 August 2022, at 14:36 (UTC).

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