Flat Absorber Coating for Spacecraft Thermal Control Applications-Reference-Cited by-同舟云学术

Flat Absorber Coating for Spacecraft Thermal Control Applications

Published:2016-11 Issue:6 Volume:53 Page:1035-1042
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Doherty Kevin A. J.¹,Dunne Conor F.¹,Norman Andrew²,McCaul Terry³,Twomey Barry⁴,Stanton Kenneth T.¹

Affiliation:

1. University College Dublin, Belfield, Dublin 4, Ireland

2. ESA, European Space Research and Technology Centre, Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands

3. Airbus Defence & Space, Stevenage, Hertfordshire, England SG1 2AS, United Kingdom

4. ENBIO Ltd., Nova University College Dublin, Dublin 4, Ireland

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.A33490

Reference29 articles.

1. DeshpandeM. S.HaradaY. “Development of Tailorable Electrically Conductive Thermal Control Material Systems,” Illinois Inst. of Technology Research Inst., Marshall Space Flight Center, NASA/CR1998, Huntsville, AL, 1998.

2. LyngviA.RandoN.GerlachL.PeacockA. “The Solar Orbiter Thermal Design,” Science Payload and Advanced Concepts Office, ESA, European Space Research and Technology Centre IAC-05-C2.6.02, Noordwijk, The Netherlands, 2005.

3. MarsdenR.MüllerD. “Solar Orbiter: Exploring the Sun—Heliosphere Connection, Definition Study Report,” ESASRE(2011)14, Noordwijk, The Netherlands, 2011.

4. Solar Orbiter—Heat shield and system technology

5. GilmoreD. G., Spacecraft Thermal Control Handbook, Vol. 1, Aerospace Press, El Segundo, CA, 2002, pp. 139–159.

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