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- W133688402 abstract "A general analysis is given of the flight dynamics of several surface-to-air and two air-to-air missile configurations. The analysis involves three phases: vertical climb, straight and level flight, and constant altitude turn. Wind tunnel aerodynamic data and full scale missile characteristics are used where available; unknown data are estimated. For the constant altitude turn phase, a three degree of freedom flight simulation is used. Important parameters considered in this analysis are the vehicle weight, Mach number, heading angle, thrust level, sideslip angle, g loading, and time to make the turn. The actual flight path during the turn is also determined. Results are presented in graphical form." @default.
- W133688402 created "2016-06-24" @default.
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- W133688402 date "1977-05-01" @default.
- W133688402 modified "2023-09-23" @default.
- W133688402 title "Analysis and compilation of missile aerodynamic data. Volume 2: Performance analysis" @default.
- W133688402 hasPublicationYear "1977" @default.
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