2017Unpublished venueRequires access

Atomic oxygen environment analysis technology for low earth orbit spacecraft

Jing An, Zhang Wei, Yang Dongsheng

Open publisher page 4 citations

Abstract

Atomic oxygen is one of the most important environmental element impacting spacecraft performance in LEO space environment. Materials used on the surface of the spacecraft may be eroded away through the reaction of Atomic oxygen, which also causes damage to spacecraft components, seriously reducing the spacecraft's orbit life. In order to avoid over-protection, This paper proposes an atomic oxygen simulation method to calculate atomic oxygen cumulative flux of different surface on spacecraft, which considered the flight attitude and mutual occlusion effect of the spacecraft. The deviation of the simulation result from the measured data of NASA is negligible. The simulation method can be used for atomic oxygen protection design of low orbit spacecraft.

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What this paper is about

Atomic oxygen is one of the most important environmental element impacting spacecraft performance in LEO space environment. Materials used on the surface of the spacecraft may be eroded away through the reaction of Atomic oxygen, which also causes damage to spacecraft components, seriously reducing the spacecraft's orbit life. In order to avoid over-protection, This paper proposes an atomic oxygen simulation method to calculate atomic oxygen cumulative flux of different surface on spacecraft, which considered the flight attitude and mutual occlusion effect of the spacecraft. The deviation of the simulation result from the measured data of NASA is negligible. The simulation method can be used for atomic oxygen protection design of low orbit spacecraft.

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OpenAlex reports 4 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Atomic oxygen is one of the most important environmental element impacting spacecraft performance in LEO space environment. Materials used on the surface of the spacecraft may be eroded away through the reaction of Atomic oxygen, which also causes damage to spacecraft components, seriously reducing the spacecraft's orbit life. In order to avoid over-protection, This paper proposes an atomic oxygen simulation method to calculate atomic oxygen cumulative flux of different surface on spacecraft, which considered the flight attitude and mutual occlusion effect of the spacecraft. The deviation of the simulation result from the measured data of NASA is negligible. The simulation method can be used for atomic oxygen protection design of low orbit spacecraft.

Key concepts: Spacecraft, Atomic oxygen, Low earth orbit, Aerospace engineering, Oxygen, Orbit (dynamics), Aerospace materials, Space environment

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