Space traffic hazards from orbital debris mitigation strategies

被引：100

作者：

Smirnov, N. N. ^{[1
,2
]}

Kiselev, A. B. ^{[2
]}

Smirnova, M. N. ^{[2
,3
]}

Nikitin, V. F. ^{[1
,2
]}

机构：

[1] Russian Acad Sci, Sci Res Inst Syst Studies, Moscow 117218, Russia

[2] Moscow MV Lomonosov State Univ, Moscow 119992, Russia

[3] St Petersburg State Polytech Univ, St Petersburg 195251, Russia

来源：

ACTA ASTRONAUTICA | 2015年 / 109卷

基金：

俄罗斯基础研究基金会;

关键词：

Space debris; Population; Collisions; Fragmentation; Hypervelocity; Impact; Vessel; Shield; Concept;

D O I：

10.1016/j.actaastro.2014.09.014

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The paper gives coverage of recent advances in mathematical modeling of long term orbital debris evolution within the frames of continua approach. Under the approach the evolution equations contain a number of source terms responsible for the variations of quantities of different fractions of orbital debris population due to fragmentations and collisions. Mechanisms of hypervelocity collisions of debris fragments with pressurized vessels are investigated. The spacecraft shield honeycomb concept is suggested based on principles of impact energy conversion and redistribution and consumption by destroyable structures. The paper is devoted to the 100th anniversary of the founder of space debris research in Moscow State University Prof. G.A. Tyulin. (C) 2014 IAA. Published by Elsevier Ltd. All rights reserved.

引用

页码：144 / 152

页数：9

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