2008•Transactions of Beijing Institute of TechnologyRequires access

Orbital Debris Risk Assessment System

Liu You-ying

Open publisher page 3 citations

Abstract

A GUI based meteoroid and orbital debris risk assessment system(MODRAS) is developed for assessing risks to spacecraft from meteoroid and debris impact.Instance a spacecraft as an example for M/OD risk assessment is conducted.The distribution of debris flux,exposed area of spacecraft and impact data are obtained.The results show that the relative impact possibility for a spacecraft depends on the spacecraft's altitude and orbital inclination,as well as debris size.Changes in shuttle mission operations,flight rules,and flight planning were adopted to reduce meteoroid and debris risks.

About this research paper

What this paper is about

A GUI based meteoroid and orbital debris risk assessment system(MODRAS) is developed for assessing risks to spacecraft from meteoroid and debris impact.Instance a spacecraft as an example for M/OD risk assessment is conducted.The distribution of debris flux,exposed area of spacecraft and impact data are obtained.The results show that the relative impact possibility for a spacecraft depends on the spacecraft's altitude and orbital inclination,as well as debris size.Changes in shuttle mission operations,flight rules,and flight planning were adopted to reduce meteoroid and debris risks.

Why it matters

OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

A GUI based meteoroid and orbital debris risk assessment system(MODRAS) is developed for assessing risks to spacecraft from meteoroid and debris impact.Instance a spacecraft as an example for M/OD risk assessment is conducted.The distribution of debris flux,exposed area of spacecraft and impact data are obtained.The results show that the relative impact possibility for a spacecraft depends on the spacecraft's altitude and orbital inclination,as well as debris size.Changes in shuttle mission operations,flight rules,and flight planning were adopted to reduce meteoroid and debris risks.

Key concepts: Spacecraft, Meteoroid, Space debris, Debris, Aerospace engineering, Environmental science, Orbital inclination, Flight planning

Related papers

Back to paper searchBrowse research topicsOriginal source
Orbital Debris Risk Assessment System — Research Paper | ScholarLens