There is a contribution from the wing, but since missiles tend to have small static margins ( typically less than a calibre ), this is usually small.
12.
The static center of gravity margin ( c . g . margin ) or static margin is the distance between the center of gravity ( or mass ) and the neutral point.
13.
It follows that the centre of pressure must lie aft of the centre of gravity for static stability . x _ { cp } is the static margin and must be negative for longitudinal static stability.
14.
In aircraft analysis, static margin is defined as the distance between the center of gravity and the neutral point of the aircraft, expressed as a percentage of the mean aerodynamic chord of the wing.
15.
If the center of gravity is behind the neutral point, the aircraft is longitudinally unstable ( the static margin is negative ), and active inputs to the control surfaces are required to maintain stable flight.
16.
The amount of static margin is an important factor in determining the handling qualities of an aircraft . For an unguided rocket, the vehicle must have a large positive static margin so the rocket shows minimum tendency to diverge from the direction of flight given to it at launch.
17.
The amount of static margin is an important factor in determining the handling qualities of an aircraft . For an unguided rocket, the vehicle must have a large positive static margin so the rocket shows minimum tendency to diverge from the direction of flight given to it at launch.
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