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|  T-45C TS, ADV & IUT ACMFP-01
Introduction to ACM
(3) At constant TAS, as G is increased so does
AOA
(4) Radial G — determines turn radius and rate
(5) Instantaneous G
(a) Maximum lift a wing may generate at a
given airspeed
(b) Dependent upon aircraft airframe/wing
(c) Displayed on velocity load factor (V n)
diagram
(d) ACM relationship — used to generate
maximum rate of turn
(6) Sustained G
(a) A function of aircraft thrust available
with respect to wing loading
(b) Maximum G capability in level turn with
constant airspeed
(c) Increases with higher thrust-to-weight
ratio
(d) ACM relationship — to maintain
energy throughout an engagement
e.
Turn radius
(1) Distance that aircraft displaces laterally in
turn
(2) Dependent on TAS and G with constant
altitude — TAS2/G
(3) TAS has a greater effect on turn radius
than rate
(05-98) Change 1
Page 1-9
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