Ablative Thermal Protection Structure Design of Ballistic Reentry Spacecraft,
FOREIGN AEROSPACE SCIENCE AND TECHNOLOGY CENTER WRIGHT-PATTERSON AFB OH
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The paper presents the ablative thermal protection structure design of a ballistic reentry spacecraft. The concepts, material selection, design approach, analytical computation and evaluation are described. Thermal protection structure, ablative material, ballistic reentry spacecraft and design.
- Spacecraft Trajectories and Reentry