This paper presents viewgraphs on the development of a non-ablative thermal management coating used as the thermal protection system material for space shuttle rocket boosters and other launch vehicles. The topics include: (1) Coating Study; (2) Aerothermal Testing; (3) Preconditioning Environments; (4) Test Observations; (5) Lightning Strike Test Panel; (6) Test Panel After Impact Testing; (7) Thermal Testing; and (8) Mechanical Testing.
Thermal Management Coating as Thermal Protection System for Space Transportation System
2002
20 pages
Report
Keine Angabe
Englisch
TRANSPORTATION DEVICE AND THERMAL MANAGEMENT SYSTEM AND THERMAL MANAGEMENT METHOD THEREFOR
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