Author: J. E. GILLIGAN
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Development of Space Stable Thermal Control Coatings for Use in Large Space Vehicles
Author: J. E. GILLIGAN
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Development of Space Stable Thermal Control Coatings for Use on Large Space Vehicles
Author: J. E. GILLIGAN
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Solar Absorptance and Thermal Emittance of Some Common Spacecraft Thermal-control Coatings
Author: John H. Henninger
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 56
Book Description
Preparation of Pigments For Space-Stable Thermal Control Coatings
Author: W. B. CAMPBELL
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 35
Book Description
Space Stable Thermal Control Coatings
Author: R. J. Mell
Publisher:
ISBN:
Category :
Languages : en
Pages : 177
Book Description
An important aspect of satellite operation in a space environment is thermal control design. Various coatings having desired optical properties have been used to achieve passive thermal control of different spacecraft. IITRI's S13G/LO coating has found widespread use in a number of missions for 15 years. The source of binder material for S13G/LO, however, is now unavailable and there is a continuing need on various spacecraft missions for this type of coating was to display desirable and reliable behavior in a space environment. The study has resulted in a material designated, S13G/LO-, however, is now unavailable and there is a continuing need on various spacecraft missions for this type of coating. This report covers research to develop and qualify a material having the same or improved optical and physical properties as S13G/Lo. The coating was to display desirable and reliable behavior in a space environment. The study has resulted in a material designated, S13G/Lo-1, which exhibits properties as good as, or somewhat better than the original S13G/LO. Keywords: Coatings, Space Environment, Satellite Thermal Control, Radiation Effects, Material Outgassing, Silicone Resin.
Publisher:
ISBN:
Category :
Languages : en
Pages : 177
Book Description
An important aspect of satellite operation in a space environment is thermal control design. Various coatings having desired optical properties have been used to achieve passive thermal control of different spacecraft. IITRI's S13G/LO coating has found widespread use in a number of missions for 15 years. The source of binder material for S13G/LO, however, is now unavailable and there is a continuing need on various spacecraft missions for this type of coating was to display desirable and reliable behavior in a space environment. The study has resulted in a material designated, S13G/LO-, however, is now unavailable and there is a continuing need on various spacecraft missions for this type of coating. This report covers research to develop and qualify a material having the same or improved optical and physical properties as S13G/Lo. The coating was to display desirable and reliable behavior in a space environment. The study has resulted in a material designated, S13G/Lo-1, which exhibits properties as good as, or somewhat better than the original S13G/LO. Keywords: Coatings, Space Environment, Satellite Thermal Control, Radiation Effects, Material Outgassing, Silicone Resin.
Spacecraft Thermal Control Coatings References
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721153459
Category :
Languages : en
Pages : 130
Book Description
The successful thermal design of spacecraft depends in part on a knowledge of the solar absorption and hemispherical emittance of the thermal control coatings used in and on the spacecraft. Goddard Space Flight Center has had since its beginning a group whose mission has been to provide thermal/optical properties data of thermal control coatings to thermal engineers. This handbook represents a summary of the data and knowledge accumulated over many years at GSFC. Kauder, Lonny Goddard Space Flight Center
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721153459
Category :
Languages : en
Pages : 130
Book Description
The successful thermal design of spacecraft depends in part on a knowledge of the solar absorption and hemispherical emittance of the thermal control coatings used in and on the spacecraft. Goddard Space Flight Center has had since its beginning a group whose mission has been to provide thermal/optical properties data of thermal control coatings to thermal engineers. This handbook represents a summary of the data and knowledge accumulated over many years at GSFC. Kauder, Lonny Goddard Space Flight Center
A Space Environment Text Chamber to Determine the Stability of Thermal Control Coatings
Author: Richard E. Gannon
Publisher:
ISBN:
Category : Heat resistant materials
Languages : en
Pages : 8
Book Description
Publisher:
ISBN:
Category : Heat resistant materials
Languages : en
Pages : 8
Book Description
Effects of Space Exposure on Thermal Control Coatings
Author: Roger C. Linton
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Evaluation of Selected Thermal Control Coatings for Long-life Space Structures
Author: Louis A. Teichman
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
Book Description
Assessment of Thermal Control and Protective Coatings
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781720387794
Category :
Languages : en
Pages : 54
Book Description
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
Publisher: Createspace Independent Publishing Platform
ISBN: 9781720387794
Category :
Languages : en
Pages : 54
Book Description
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