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Posted (edited)

Alright, time to get nerdy.

Taken from T.O. 1F-5E-1-1984_OCR

14be79d54535a7ec77091e9acb4d280e.png

4f0f28eaf1712ca1d5c249fc02b7d901.png

 

I understand how to work with this graphic, however it works only for takeoff considering the index point includes a/c, pilot, full internal fuel, launcher rails, and no ammo.

 

How can I calculate/estimate the CG position after takeoff at any point of the flight? More specifically at final approach and landing.

How can I adjust for the reduction of gross weight in the index point?

Is there any rule of thumb?

 

I don't plan on taking out the graph mid flight to do the calculations, it's for mission planning purposes.

Edited by Kimi_uy
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