GuardianRED
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Yes we all know how to use Google !!!!.... Thank youthrust has to be proportional to weight that's thrust:weight which in case of an LV changes due to dM (change in mass) and rapid acceleration which are inversely proportional to eachother f*m =1/dv/dt. You have to use differential equation to calculate the exact using Hamiltonian and holonomic coordinates in 3D scenario considering the Coriolis's force -2mwv which is due to earth's gravitation and rotation when an object moves into parabolic flight..
lift to drag ratio depends on angle of attack area of the wing/sphere more over the air velocity above the body and below the body we sometimes calculate the drag as gradient of air velocity behind the wing.. where aerodynamic lift is propotional to change in pressure times area
for nonsymmetric object we consider the lift as dynamic lift
sensor fusion is nothing but a system which refines the data
high bypass low by pass ducts are nothing but other definition of generating high bypass pressure and low by pass pressure 10:6 for every 10kg of air in low 6 kg bypasses in high..
all those parts are the parts of a profile ..
We can see that you are new here.... Still it plays to do SOME research on the topic of the thread before commenting ....source?
There is A Sticky Thread dedicated to Indian Missile and its systems , where most of the post here, was posted there much earlier - Please do see that, it is a good read