An investigation of the protection afforded a spacecraft by a thin shield

Author:

MAIDEN C.1,MCMILLAN A.2

Affiliation:

1. GENERAL MOTORS CORP., DEFENSE RESEARCH LABS., STRUCTURAL DYNAMICS GROUP, SANTA BARBARA, CALIF.

2. GENERAL MOTORS CORP., DEFENSE RESEARCH LABS., HIGH VELOCITY IMPACT GROUP, SANTA BARBARA, CALIF.

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A theoretical and numerical study on the perforation of thin metallic plates by high speed long rods;Mechanics Based Design of Structures and Machines;2021-03-12

2. Development of Ballistic Limit Equations for Dual-Wall Spacecraft Shielding: A Concise History and Suggestions for Future Development;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

3. EFFECTIVENESS OF METEOROID BUMPERS COMPOSED OF TWO LAYERS OF DISTINCT MATERIALS;8th Structural Dynamics and Materials Conference;1967-03-29

4. Hypervelocity impact studies concerning the meteoroid hazard to aerospace materials and structures (Meteoroid hazard to spacecraft materials and structures, using particle-projection techniques);5th Annual Structures and Materials Conference;1964-04

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