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Preliminary Design and Experimental Investigation of the FDL-5A Unmanned High L/D Spacecraft. Part 2. Parametric Configuration Development and Evaluation

机译:FDL-5a无人高L / D航天器的初步设计与实验研究。第2部分。参数配置开发和评估

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The derivation of two volumetric efficient high L/D entry vehicles is described. Parametric trades in the areas of aerodynamics and aerothermodynamics are discussed and selected parameters are identified. Alternate modes of vehicle recovery are described and the effect on vehicle design determined. The evolution of the FDL-5 configuration selected for wind tunnel testing is described through the presentation of a series of intermediate configurations. (Author)

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