Testing and Optimization of Electrically Conductive Spacecraft Coatings Final Report ... Nasa

Testing and Optimization of Electrically Conductive Spacecraft Coatings Final Report ... Nasa PDF Author: United States. National Aeronautics and Space Administration
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Languages : en
Pages :

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Testing and Optimization of Electrically Conductive Spacecraft Coatings Final Report ... Nasa

Testing and Optimization of Electrically Conductive Spacecraft Coatings Final Report ... Nasa PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Testing and Optimization of Electrically Conductive Spacecraft Coatings

Testing and Optimization of Electrically Conductive Spacecraft Coatings PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781723894626
Category :
Languages : en
Pages : 62

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This is the final report discussing the work done for the Space Environments and Effects (SEE) Program. It discusses test chamber design, coating research, and test results on electrically thermal control coatings. These thermal control coatings are being developed to have several orders of magnitude higher electrical conductivity than most available thermal control coatings. Most current coatings tend to have a range in surface resistivity from 1,011 to 1,013 ohms/sq. Historically, spacecraft have had thermal control surfaces composed of dielectric materials of either polymers (paints and metalized films) or glasses (ceramic paints and optical solar reflectors). Very seldom has the thermal control surface of a spacecraft been a metal where the surface would be intrinsically electrically conductive. The poor thermal optical properties of most metals have, in most cases, stopped them from being used as a thermal control surface. Metals low infrared emittance (generally considered poor for thermal control surfaces) and/or solar absorptance, have resulted in the use of various dielectric coatings or films being applied over the substrate materials in order to obtain the required optical properties.Mell, R. J. and Wertz, G. E. and Edwards, D. L. (Technical Monitor)Marshall Space Flight CenterCONTROL SURFACES; ELECTRICAL RESISTIVITY; TEMPERATURE CONTROL; THERMAL CONTROL COATINGS; DIELECTRICS; CERAMICS

Testing and Optimization of Electrically Conductive Spacecraft Coatings

Testing and Optimization of Electrically Conductive Spacecraft Coatings PDF Author: R. J. Mell
Publisher:
ISBN:
Category : Protective coatings
Languages : en
Pages : 64

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NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 478

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A Selected Listing of NASA Scientific and Technical Reports

A Selected Listing of NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 470

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Assessment of Thermal Control and Protective Coatings

Assessment of Thermal Control and Protective Coatings PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781720387794
Category :
Languages : en
Pages : 54

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This final report is concerned with the tasks performed during the contract period which included spacecraft coating development, testing, and applications. Five marker coatings consisting of a bright yellow handrail coating, protective overcoat for ceramic coatings, and specialized primers for composites (or polymer) surfaces were developed and commercialized by AZ Technology during this program. Most of the coatings have passed space environmental stability requirements via ground tests and/or flight verification. Marker coatings and protective overcoats were successfully flown on the Passive Optical Sample Assembly (POSA) and the Optical Properties Monitor (OPM) experiments flown on the Russian space station MIR. To date, most of the coatings developed and/or modified during this program have been utilized on the International Space Station and other spacecraft. For ISS, AZ Technology manufactured the 'UNITY' emblem now being flown on the NASA UNITY node (Node 1) that is docked to the Russian Zarya (FGB) utilizing the colored marker coatings (white, blue, red) developed by AZ Technology. The UNITY emblem included the US American flag, the Unity logo, and NASA logo on a white background, applied to a Beta cloth substrate.Mell, Richard J.Marshall Space Flight CenterPROTECTIVE COATINGS; THERMAL CONTROL COATINGS; OPTICAL PROPERTIES; COLOR

Solar Absorptance and Thermal Emittance of Some Common Spacecraft Thermal-control Coatings

Solar Absorptance and Thermal Emittance of Some Common Spacecraft Thermal-control Coatings PDF Author: John H. Henninger
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 56

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Technology for Large Space Systems

Technology for Large Space Systems PDF Author:
Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 172

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

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Solar Energy Update

Solar Energy Update PDF Author:
Publisher:
ISBN:
Category : Solar energy
Languages : en
Pages : 874

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