Thermal Optical Properties of Plasma-Sprayed Mullite Coatings for Space Launch Vehicles
Author:
Affiliation:
1. Technische Universitat Bergakademie Freiberg, D-09596 Freiberg, Germany
2. Integrity Testing Laboratory, Inc., Markham, Ontario L3R 2R7, Canada
3. Oceangate Consulting, D-34346 Hann.Munden, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.14568
Reference24 articles.
1. Spacecraft Thermal Control Handbook;Gilmore D. G.,2002
2. Effect of low earth orbit atomic oxygen on spacecraft materials
3. 5Seifert, S. "Development of Ceramic Lightweight Thermal Protection Coatings for Reusable Space Launch Vehicles," Unpublished M.S. Thesis,Technische Universität Bergakademie Freiberg, Freiberg, Germany, June 2004.
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