F-22 PW-100 Engine
#1
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From: NorthEast,
NJ
Anyone know a website where I may be able to get some specifics on this engine? Looking for length, diameter, fuel consumption, weight and stuff like that.
Thanks Guys!
Thanks Guys!
#2

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From: Los Angeles
ORIGINAL: EricJ
Anyone know a website where I may be able to get some specifics on this engine? Looking for length, diameter, fuel consumption, weight and stuff like that.
Thanks Guys!
Anyone know a website where I may be able to get some specifics on this engine? Looking for length, diameter, fuel consumption, weight and stuff like that.
Thanks Guys!
#3

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From: Los Angeles
More specifically...

http://www.allstar.fiu.edu/aero/P&WEngines04.html
http://www.f22fighter.com/engines.htm
Couldn't find any in depth specs on the engine itself yet.

http://www.allstar.fiu.edu/aero/P&WEngines04.html
http://www.f22fighter.com/engines.htm
Couldn't find any in depth specs on the engine itself yet.
#4
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From: Anchorage,
AK
Check out this link, with image, at http://www.f-22raptor.com/af_engines.php It comes from http://www.f-22raptor.com
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From: HADLEY,
MA
HERE IS SOME INFO FOR YOU,NOT MUCH BUT THIS IS WHAT I HAVE.IT IS A TWIN SPOOL,AUGMENTED TURBOFAN 35,000 POUND THRUST CLASS.IT HAS A THREE STAGE FAN AND A SIX STAGE COMPRESSOR.THE COMBUSTOR IS ANNULAR.THE TURBINE IS AXIAL FLOW/COUNTER ROTATING WITH ONE STAGE HIGH PRESSURE AND ONE STAGE LOW PRESSURE.THE NOZZLE IS A TWO DIMENSIONAL VECTORING CONVERGENT/DIVERGENT.THIS ENGINE WAS ALSO SELECTED TO POWER THE F-22 BACK IN APRIL 1991.FIRST FLIGHT WAS 1997.THIS PROBABLY IS NOT WHAT YOU ARE LOOKING FOR BUT HERE IT IS,I ALSO HAVE A PICTURE OF THE ENGINE CUT-AWAY IF YOU WOULD LIKE.



