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To: MtnClimber

The Pratt & Whitney J58 documentation for that application covered a range of figures up to Mach 4.2, coordinating altitude, range, fuel burn rate, power derating based on altitude above FL72, etc. The chart curves indicated Mach ~3.2 gave the best range.


132 posted on 12/29/2016 10:15:38 AM PST by Ozark Tom
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To: Ozark Tom

https://www.nasa.gov/centers/dryden/pdf/88507main_H-2179.pdf

http://www.ga153.com/aero%20space/Aero%20space%20information%20page/aircraft/SR.pdf


136 posted on 12/29/2016 11:57:48 AM PST by Ozark Tom
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To: Ozark Tom
"...The Pratt & Whitney J58 documentation for that application covered a range of figures up to Mach 4.2, coordinating altitude, range, fuel burn rate, power derating based on altitude above FL72, etc. The chart curves indicated Mach ~3.2 gave the best range....." Ah Yes! Here's my little souvenir from the early '60s that the engine development team had at the time. Even the coffee cups were classified back then.  photo DSC_0035_zpserryupuq.jpg
144 posted on 12/30/2016 1:07:15 AM PST by lgjhn23 (It's easy to be liberal when you're dumber than a box of rocks.)
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