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Landing-gear weight equation

The landing-gear WERs typically used for manned
aircraft can be used within their applicable range for unmanned aircraft.

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Gross Thrust Coefficient

The gross thrust coefficient (Cfg) is a measure of the nozzle efficiency and accounts for nozzle losses due to friction, angularity, expansion, leakage and cooling air throttling

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Down Stream Mach Number

The Mach number of a normal shock wave is always greater than unity in the upstream and less than unity in the downstream, the static pressure always increases across the shock wave

Mx= Up Stream Mach Number

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Frequency Parameter calculator

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pitch rate calculator

The pitch rate of an aircraft is a rate of change of the aircraft orientation with respect to an inertial frame, expressed in body axes