Accession Number : ADA256908


Title :   Ablative Thermal Protection Structure Design of Ballistic Reentry Spacecraft,


Corporate Author : FOREIGN AEROSPACE SCIENCE AND TECHNOLOGY CENTER WRIGHT-PATTERSON AFB OH


Personal Author(s) : Qinghua, Chen


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a256908.pdf


Report Date : Oct 1992


Pagination or Media Count : 14


Abstract : 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.


Descriptors :   *THERMAL PROPERTIES , *REENTRY VEHICLES , *SPACECRAFT , COMPUTATIONS , MATERIALS , STRUCTURES , PROTECTION , TRANSLATIONS , BALLISTICS , SELECTION , CHINA , ABLATIVE MATERIALS , APPROACH


Subject Categories : Thermodynamics
      Spacecraft Trajectories and Reentry


Distribution Statement : APPROVED FOR PUBLIC RELEASE