Arcjet Testing and Thermal Model Development for Multilayer Felt Reusable Surface InsulationFelt Reusable Surface Insulation was used extensively on leeward external surfaces of the Shuttle Orbiter, where the material is reusable for temperatures up to 670 K. For application on leeward surfaces of the Orion Multi-Purpose Crew Vehicle, where predicted temperatures reach 1620 K, the material functions as a pyrolyzing conformal ablator. An arcjet test series was conducted to assess the performance of multilayer Felt Reusable Surface Insulation at high temperatures, and a thermal-response, pyrolysis, and ablation model was developed. Model predictions compare favorably with the arcjet test data
Document ID
20120016059
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Milos, Frank S. (NASA Ames Research Center Moffett Field, CA, United States)
Scott, Carl Douglas (Jacobs Technology, Inc. Moffett Field, CA, United States)
Papa, Steven V. (NASA Ames Research Center Moffett Field, CA, United States)