TY - JOUR
T1 - Flat absorber coating for spacecraft thermal control applications
AU - Doherty, Kevin A.J.
AU - Dunne, Conor F.
AU - Norman, Andrew
AU - McCaul, Terry
AU - Twomey, Barry
AU - Stanton, Kenneth T.
N1 - Publisher Copyright:
Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2016
Y1 - 2016
N2 - SolarBlack is a bone-char-based surface developed as a flat absorber (black) thermal control surface for use on spacecraft. The surface, originally developed for use on the front shield of "ESAs" Solar Orbiter, is deposited using a technique known as CoBlast, developed by ENBIO Ltd. The resulting surface makes use of the material's highly stable ratio of solar absorptance to near-normal thermal emissivity (αs/ϵN) as well as its low electrical resistivity to regulate both temperature and electrostatic dissipation in service. SolarBlack is suitable for use on rigid and flexible metallic substrates, including titanium, aluminum, copper, stainless steel, nitinol, Inconel, and magnesium alloys. This work describes the thermo-optical properties, stability, and qualification of this surface for use on spacecraft components, as well as material characterization of the coating and bone char itself. The thermooptical stability of SolarBlack was determined using the Synergistic Temperature Accelerated Radiation facility space environment simulator in the European Space Research and Technology Centre, having previously qualified for use on Solar Orbiter. Material characterization was carried out using simultaneous thermal analysis, scanning electron microscopy, ultraviolet/visible/near-infrared spectrometry, and infrared emissometry.
AB - SolarBlack is a bone-char-based surface developed as a flat absorber (black) thermal control surface for use on spacecraft. The surface, originally developed for use on the front shield of "ESAs" Solar Orbiter, is deposited using a technique known as CoBlast, developed by ENBIO Ltd. The resulting surface makes use of the material's highly stable ratio of solar absorptance to near-normal thermal emissivity (αs/ϵN) as well as its low electrical resistivity to regulate both temperature and electrostatic dissipation in service. SolarBlack is suitable for use on rigid and flexible metallic substrates, including titanium, aluminum, copper, stainless steel, nitinol, Inconel, and magnesium alloys. This work describes the thermo-optical properties, stability, and qualification of this surface for use on spacecraft components, as well as material characterization of the coating and bone char itself. The thermooptical stability of SolarBlack was determined using the Synergistic Temperature Accelerated Radiation facility space environment simulator in the European Space Research and Technology Centre, having previously qualified for use on Solar Orbiter. Material characterization was carried out using simultaneous thermal analysis, scanning electron microscopy, ultraviolet/visible/near-infrared spectrometry, and infrared emissometry.
UR - http://www.scopus.com/inward/record.url?scp=85012201568&partnerID=8YFLogxK
U2 - 10.2514/1.A33490
DO - 10.2514/1.A33490
M3 - Article
AN - SCOPUS:85012201568
SN - 0022-4650
VL - 53
SP - 1035
EP - 1042
JO - Journal of Spacecraft and Rockets
JF - Journal of Spacecraft and Rockets
IS - 6
ER -