F100 & F110 engines installed performance

Jacky

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Hi gays. There is a Fig that shows the installed performance of F100(I guess it's F100-PW-200/220) in the paper" A FLIGHT THRUST DECK FOR THE F100 TURBOFAN OF THE F-16 AIRCRAFT" ?

Do anyone have information about installed performance of F110-GE-100 engine? 83GI@S[MZ%H{()@7{`RW]7E.png
 
Yes funny enough, in an old Key topic
 

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HFFM data by Mav-JP and Raptor one

The upgraded F-14A+, later redesignated F-14B, and F-14D were equipped with the General Electric F110-GE-400. The F110 provided a significant increase in thrust, with a static uninstalled thrust of 28,000 pounds-force (125 kN); installed thrust is 23,400 pounds-force (104 kN) with afterburner at sea level, which rose to 30,200 lbf (134 kN) at Mach 0.9
Wikipedia citing
  • NAVAIR 01-F-14AAD-1A F-14D NATOPS FLIGHT MANUAL January 2004 PART 1 CH-2 Section 2.2 "Engine" pg "2–9".
 

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F100-pw-229, RD-33, R-35, Al-31f, and WS-10A
Along with another version of the F100-pw-200.


I figure since I already posted a bunch here this would be a good place for them that way you have ease of comparison. The AL-31f and WS-10a are installed in Flankers. All the F100 and F110 curves I e posted except the blue one are installed in a Viper.
 

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Hey,
I was wondering if anyone here had thrust graphs for the F110-GE-400 installed in an F-14B/D. Thanks in advance!
 

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