This thesis is comprised of four independent computer programs and their related operating instructions. Each of these programs focuses on a particular facet of tactical missile design. The topics covered include guidance and trajectory calculations, rocket motor propulsion sizing, warhead design, and aerodynamic coefficient determination. The programs are developed from accepted mathematical procedures and are tailored to optimize operator interaction for educational purposes.
Computer Program Applications to Tactical Missile Conceptual Design
1981
200 pages
Report
No indication
English
Missile Technology , Guided missiles , Tactical warfare , Computer aided design , Guidance computers , Guided missile warheads , Aerodynamic characteristics , Coefficients , Threats , Missions , Computerized simulation , Mathematical models , Military planning , Theses , Aerol computer program , IBM 370 computers
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