M/OD risk assessment system and its applications

Hai Fu Wang; Qing Bo Yu; You Ying Liu; Hui Wang

M/OD risk assessment system and its applications

Hai Fu Wang^*, Qing Bo Yu, You Ying Liu, Hui Wang

^*Corresponding author for this work

School of Mechatronical Engineering

Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Abstract

A risk assessment system named meteoroid & orbital debris risk assessment system (MODRAS) developed for assessing risks of the spacecraft under the meteoroid and debris environment (M/OD EM) is presented. The computing resolution of MODRAS has been verified by both the three generic spacecraft geometries of inter agency debris committee (IADC) and similar foreign software such as BUMPER, ESABASE, and MDPANTO. The results show that the system is fit well with the computing results of the foreign software. Typical applications of the system are also presented, including a manned spacecraft and a space shuttle.

Original language	English
Pages (from-to)	6-10
Number of pages	5
Journal	Journal of Beijing Institute of Technology (English Edition)
Volume	18
Issue number	1
Publication status	Published - Mar 2009

Keywords

Finite element model
Impact risk
Orbital debris
Spacecraft

Cite this

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abstract = "A risk assessment system named meteoroid & orbital debris risk assessment system (MODRAS) developed for assessing risks of the spacecraft under the meteoroid and debris environment (M/OD EM) is presented. The computing resolution of MODRAS has been verified by both the three generic spacecraft geometries of inter agency debris committee (IADC) and similar foreign software such as BUMPER, ESABASE, and MDPANTO. The results show that the system is fit well with the computing results of the foreign software. Typical applications of the system are also presented, including a manned spacecraft and a space shuttle.",

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AU - Yu, Qing Bo

AU - Liu, You Ying

AU - Wang, Hui

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N2 - A risk assessment system named meteoroid & orbital debris risk assessment system (MODRAS) developed for assessing risks of the spacecraft under the meteoroid and debris environment (M/OD EM) is presented. The computing resolution of MODRAS has been verified by both the three generic spacecraft geometries of inter agency debris committee (IADC) and similar foreign software such as BUMPER, ESABASE, and MDPANTO. The results show that the system is fit well with the computing results of the foreign software. Typical applications of the system are also presented, including a manned spacecraft and a space shuttle.

AB - A risk assessment system named meteoroid & orbital debris risk assessment system (MODRAS) developed for assessing risks of the spacecraft under the meteoroid and debris environment (M/OD EM) is presented. The computing resolution of MODRAS has been verified by both the three generic spacecraft geometries of inter agency debris committee (IADC) and similar foreign software such as BUMPER, ESABASE, and MDPANTO. The results show that the system is fit well with the computing results of the foreign software. Typical applications of the system are also presented, including a manned spacecraft and a space shuttle.

KW - Finite element model

KW - Impact risk

KW - Orbital debris

KW - Spacecraft

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JF - Journal of Beijing Institute of Technology (English Edition)

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M/OD risk assessment system and its applications

Abstract

Keywords

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