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Development of a Total Trajectory Simulation for Single Recovery Parachute Systems. Volume I. Analytical Model and Computer Program Design Rationale.

机译:单回收降落伞系统全弹道仿真的研制。第一卷。分析模型和计算机程序设计原理。

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A method of total trajectory simulation was established which is based on the governing equations of the various phases of an airdrop or recovery system. In view of these equations, a computer program capable of predicting the performance characteristics of a parachute-load system from the instant of initiation to the moment of landing was established. Calculations were performed for a number of different aerial delivery systems. The calculated results fall well within the broad ranges of expected performance,based upon a familiarity with field test results. (Modified author abstract)

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