The effects that specified delays in activating the thrust and control system have on the altitude history of a TIGER-II vehicle released from an F-4 and F-111 were analyzed using a three degree-of-freedom analog simulation. Desirable delay times were identified that would allow acceptable ground clearance when releasing from 100-ft altitude. The effect that atmospheric turbulence had on the vehicle was considered for the defined time delays. (ERA citation 05:012272)
Effects of Turbulence and Delay in Activating TIGER II after Low Altitude Release
1979
25 pages
Report
Keine Angabe
Englisch
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