DESIGN AND PERFORMANCE EQUATIONS FOR ADVANCED METEOROID AND DEBRIS SHIELDS

被引：208

作者：

CHRISTIANSEN, EL

机构：

[1] NASA Johnson Space Center, Houston, TX 77058

来源：

INTERNATIONAL JOURNAL OF IMPACT ENGINEERING | 1993年 / 14卷 / 1-4期

关键词：

Aluminum - Equations of state - Impact resistance - Mathematical models - Space debris;

D O I：

10.1016/0734-743X(93)90016-Z

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

This paper provides equations defining the performance capability of various types of meteoroid and debris shielding systems. These equations have been developed at the NASA Johnson Space Center (JSC) Hypervelocity Impact Test Facility (HIT-F). Equations are included that are applicable for aluminum Whipple shields, Nextel(R) Multi-Shock (MS) shields, hybrid Nextel(R)/Aluminum MS shields, and Mesh Double-Bumper (MDB) shields. The MS and MDB shields are advanced shields with demonstrated weight and performance advantages over conventional Whipple shields.

引用

页码：145 / 156

页数：12