HercFan

Does anyone have numbers for the test stand maximum static thrust for the various engine and prop combinations used on the Herc over the years? I'm interested in doing some theoretical comparitive takeoff performance calculations for the standard USAF Herc models A,B,E,H,and J. The method I'm using is based on some simplified thrust-to-weight equations and works better with actual test stand results than by using the handbook spec figures for shp and torque. Am particularly interested in the A,E,&H all of which I flew. Thanks