DATCOMData Compendium (US Air Force)
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[15], and Pontani [16], the aerodynamics of the rocket was modeled through the Missile DATCOM software [13].
This means that DATCOM was run 3024 times for each (l, d) combination.
The drag coefficient ([C.sub.D]) and lift coefficient ([C.sub.L]), calculated by using Missile DATCOM, were arranged in lockup tables.