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.
Ablative Thermal Protection Structure Design of Ballistic Reentry Spacecraft
1992
14 pages
Report
Keine Angabe
Englisch
Ablative Protective Material for Reentry Bodies
NTIS | 1975
|Multi-Fidelity Design of an Integrated Thermal Protection System for Spacecraft Reentry
British Library Conference Proceedings | 2008
|