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- W114689036 abstract "This chapter focuses on computer programs for space missions. The proper determination of the design and performance characteristics of missile systems requires an analysis which would introduce and account for the complicated interactions among a large number of significant parameters. Such an analysis must take into account such features as the component weights and stages of the missile structure, the environmental conditions of atmospheric properties and winds, the material factors of densities, stresses, specific heats, and the like, and the propulsive properties such as thrust direction and magnitude all subject to the physical laws governing the trajectory. The usual method of determining near optimum values of the important system parameters for a given mission is a trial and error method requiring repeated use of a basic computer program and resulting in curves showing the interactions of various parameters. For a given missile configuration and a preassigned launch-site-target combination, the objective of a missile simulation program is to determine certain parameters of the dynamical and guidance systems which will result in the impact." @default.
- W114689036 created "2016-06-24" @default.
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- W114689036 date "1960-01-01" @default.
- W114689036 modified "2023-09-27" @default.
- W114689036 title "Computer Programs for Space Missions" @default.
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- W114689036 doi "https://doi.org/10.1016/b978-1-4832-2736-8.50012-3" @default.
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