Title page for ETD etd-07152010-020313


Type of Document Master's Thesis
Author Halter, Megaera C.
URN etd-07152010-020313
Title Energy-turns analysis for a scramjet powered missle
Degree Master of Science
Department Aerospace Engineering
Advisory Committee
Advisor Name Title
Cliff, Eugene M. Committee Chair
Lutze, Frederick H. Jr. Committee Member
Marchman, James F. III Committee Member
Keywords
  • Guided missiles
Date of Defense 1988-05-15
Availability restricted
Abstract

A reduced order model describing the energy and heading angle dynamics of a scramjet missile is developed using a singular perturbation technique. The cruise analysis is briefly reviewed to determine the conditions at which the missile will cruise most efficiently. The turn and climb performance of the missile over the conditions of interest is then examined and a family of extremal trajectories is constructed which asymptotically approach the cruise at an intermediate altitude.

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