Configuration which employs winged payload and stabilizing fins at rear of booster will develop sizable rolling moments due to winds during ascent which exceed control authority of vehicle; analysis of modification of control system configuration to minimize rolling moments; summary of significant aspects of roll control problem.
Roll control problem of finned rocket vehicles with winged payloads
Aerospace Eng
Aerospace Engineering ; 21 , n 11 ; p 58-59 + 83
1962
Article (Journal)
English
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