1991•Journal of Vacuum Science & Technology A Vacuum Surfaces and FilmsRequires access

Space simulation for the study of material outgassing

Lloyd B. Gordon, Jon C Little, Robert G. Phillips

Open publisher page 6 citations

Abstract

The design of a system to study the outgassing characteristics of materials under a simulated space environment is described. A vacuum chamber simulates the pressure experienced by spacecraft in earth orbit and on the lunar surface. The samples are mounted on a cold/hot surface whose temperature can be varied between −200 and +200 °C. Windows allow the application of ultraviolet radiation. The pressure in the chamber and the material temperatures are monitored, and the outgassing products are analyzed with a quadrupole mass spectrometer. A specially designed sampling system allows the mass spectrometer to automatically measure gases in the simulation chamber for a wide range of dynamically varying pressures. Applications of the space simulation chamber to dielectric-material outgassing characterization under the space environment conditions are discussed.

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What this paper is about

The design of a system to study the outgassing characteristics of materials under a simulated space environment is described. A vacuum chamber simulates the pressure experienced by spacecraft in earth orbit and on the lunar surface. The samples are mounted on a cold/hot surface whose temperature can be varied between −200 and +200 °C. Windows allow the application of ultraviolet radiation. The pressure in the chamber and the material temperatures are monitored, and the outgassing products are analyzed with a quadrupole mass spectrometer. A specially designed sampling system allows the mass spectrometer to automatically measure gases in the simulation chamber for a wide range of dynamically varying pressures. Applications of the space simulation chamber to dielectric-material outgassing characterization under the space environment conditions are discussed.

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Available abstract

The design of a system to study the outgassing characteristics of materials under a simulated space environment is described. A vacuum chamber simulates the pressure experienced by spacecraft in earth orbit and on the lunar surface. The samples are mounted on a cold/hot surface whose temperature can be varied between −200 and +200 °C. Windows allow the application of ultraviolet radiation. The pressure in the chamber and the material temperatures are monitored, and the outgassing products are analyzed with a quadrupole mass spectrometer. A specially designed sampling system allows the mass spectrometer to automatically measure gases in the simulation chamber for a wide range of dynamically varying pressures. Applications of the space simulation chamber to dielectric-material outgassing characterization under the space environment conditions are discussed.

Key concepts: Outgassing, Quadrupole mass analyzer, Spacecraft, Vacuum chamber, Space environment, Spectrometer, Thermal emittance, Materials science

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