Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Development  





2 Specifications  





3 References  



3.1  Citations  





3.2  Bibliography  
















De Havilland DH.15






Deutsch
فارسی
Français
Italiano
Тоҷикӣ
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 




In other projects  



Wikimedia Commons
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


DH.15
Role Engine test bed
National origin United Kingdom
Manufacturer The Aircraft Manufacturing Co. Ltd.
Status abandoned
Number built 1
Developed from de Havilland DH.9A

The de Havilland DH.15 Gazelle was an engine testbed for the B.H.P Atlantic engine, converted from a de Havilland DH.9A for flight trials in 1919–20. Only one was built.

Development[edit]

The DH.15 Gazelle, more often known just as the DH.15, was a standard DH.9A, complete with original armament, converted for use as an engine testbed.[1] The engine involved was the 500 hp (373 kW) B.H.P. Atlantic, a water-cooled V-12 unit produced by the Galloway Engineering Co., which merged two six-cylinder inline B.H.P. engines onto a common crankcase. This replaced the DH.9A's standard 400 hp (300 kW) Liberty 12, although without a great change in appearance, as the Atlantic was mounted behind a similar large rectangular radiator. Both engines were upright V-12s, both with crankshafts near the base, and in each case, the propeller was mounted low on the nose. The exhaust pipes on the DH.15 were longer than the usual DH.9A set, running straight back from the upper sides of the engine, ending at the observer's cockpit.[1]

Two DH.15s were ordered, but only one was built. It completed many flights with the Atlantic engine from 1919 to 1920.[1]

Specifications[edit]

Data from [1]

General characteristics

Performance

Armament

References[edit]

Citations[edit]

  1. ^ a b c d Jackson 1978, p. 153
  • ^ Mason 1994, p. 129
  • Bibliography[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=De_Havilland_DH.15&oldid=1210243737"

    Categories: 
    1910s British experimental aircraft
    De Havilland aircraft
    Airco aircraft
    Single-engined tractor aircraft
    Biplanes
    Aircraft first flown in 1919
    Hidden categories: 
    Use dmy dates from January 2018
    Use British English from January 2018
    Articles needing additional references from December 2015
    All articles needing additional references
    Articles with short description
    Short description is different from Wikidata
    Commons category link from Wikidata
     



    This page was last edited on 25 February 2024, at 17:58 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki