Open main menu
Home
Random
Recent changes
Special pages
Community portal
Preferences
About Wikipedia
Disclaimers
Incubator escapee wiki
Search
User menu
Talk
Dark mode
Contributions
Create account
Log in
Editing
Hawker Tempest
(section)
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
=== Drawing board designs === In 1943, Camm initiated work on a new design for fighter equipped with the at that point unbuilt [[Rolls-Royce Eagle (1944)|Rolls-Royce R.46]] engine. The project designated as the ''P.1027'' was essentially a slightly enlarged Tempest with the R.46 engine, which Hawker expected to develop around 4,000 hp (2,980 kW). This engine would have driven a pair of four-bladed [[contra-rotating]] propellers. The radiator was relocated into a ventral bath set underneath the rear fuselage and wing centre section: the wingspan was {{convert|41|ft|m|abbr=on}} and the length was {{convert|37|ft|3|in|m|abbr=on}}.<ref name=buttler30/> However, work upon the P.1027 design was soon dropped in favour of concentrating upon a further developed design, the ''P.1030,'' in September It featured wing leading edge radiators and had larger overall dimensions of {{convert|42|ft|m|abbr=on}} wingspan and {{convert|39|ft|9|in|m|abbr=on}} length. The top speed was calculated as {{convert|509|mph|km/h|abbr=on}} at 20,000 ft, with a rate of climb of 6,400 ft/min (1,951 m/min). Service ceiling was projected to be more than {{convert|42,000|ft|m|abbr=on}}.<ref name=buttler30>Buttler 2004, p. 30.</ref> Work on both was ultimately dropped when Camm decided to focus design efforts upon the more promising jet engine designs he was working on instead.
Edit summary
(Briefly describe your changes)
By publishing changes, you agree to the
Terms of Use
, and you irrevocably agree to release your contribution under the
CC BY-SA 4.0 License
and the
GFDL
. You agree that a hyperlink or URL is sufficient attribution under the Creative Commons license.
Cancel
Editing help
(opens in new window)