----[Please read http://ercoupers.com/disclaimer.htm before following any advice in this forum.]----
Why would one want to burn 15 Gallons per hour just
to get 60 hp onto the prop??
Admitted the turbine would produce these sixty
horses even at 18000ft altitude, but then I would need an instrument rating plus
the expenses of the oxygen.
Also, the 20 lb engine will make my plane quiet
tail heavy...
However, nice experiment - mentally.
Hartmut
----- Original Message -----
From: Greg BulloughTo: Ed Burkhead ; Coupe-ListSent: Tuesday, November 04, 2003 4:40 PMSubject: Re: [COUPERS-FLYIN] Test aircraft needed :-)----[Please read http://ercoupers.com/disclaimer.htm before following any advice in this forum.]---- At 05:59 PM 11/4/2003 -0600, Ed Burkhead wrote:
Anyone want to be our test aircraft?
http://www.microjeteng.com/turboshaft.htm
Looks like fun...
Hint: (.9 ltr/min / .946 quarts/ltr) * 60 / 4 = 14.27 gph
Kerosene is 7 lb./gal isnt it?
Yeah, but that's at max RPM. What's it do when putting
out just 75% power and with the prop pitch optimized? And
given that the weight is so low, wouldn't you be able to
carry a bit more fuel?
Greg ============================================================================== To leave this forum go to: http://ercoupers.com/lists.htm Search the archives on http://escribe.com/aviation/coupers/
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