Inorganic White Thermal-Control Coatings for Extreme Space Environments-Reference-Cited by-同舟云学术

Inorganic White Thermal-Control Coatings for Extreme Space Environments

Published:2016-11 Issue:6 Volume:53 Page:1061-1067
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Shrestha S.¹,Borrero del Pino C.²,Malayoglu U.³

Affiliation:

1. Keronite International Limited, Haverhill, England CB9 8PJ, United Kingdom

2. Airbus DS GmbH, 81663 Ottobrunn, Germany

3. Dokuz Eylül University, Buca-Izmir 35160, Turkey

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.A33508

Reference11 articles.

1. Plasma electrolytic oxidation and anodising of aluminium alloys for spacecraft applications

2. JaworskeD. A.KlineS. E. “Review of End-of-Life Thermal Control Coating Performance,” NASA TM-2008-215173, April 2008.

3. Degradation of thermal control materials under a simulated radiative space environment

4. Plasma electrolysis for surface engineering

5. RenardE. “Process Specification for Black Micro-Arc Oxidation/Plasma Electrolytic Oxidation on Titanium and Aluminum Alloys,” Airbus Defence and Space , QTM.SP.ER.09.303, Toulouse, France, 2012.

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