被撤回的出版物: The laser-driven flyer system for space debris hypervelocity impact simulations (Retracted article. See vol. 268, pg. 1532, 2010)

NUCLEAR INSTRUMENTS & METHODS IN PHYSICS RESEARCH SECTION B-BEAM INTERACTIONS WITH MATERIALS AND ATOMS

卷:267

Article; Proceedings Paper; Retracted Publication

Gong Zizheng¹  Dai Fu¹  Cao Yan¹  Zhang Wenbing¹  Yang Jiyun¹  Tong Jingyu¹ 

[1] Beijing Inst Spacecrafts Environm Engn, Beijing 100094, Peoples R China

关键词: Laser-driven flyer system;    Hypervelocity impacts;    Micro meteoroids and orbital debris;    Cumulated damage characteristics;    The outer surfaces functional material;    Spacecraft;   

DOI  :  10.1016/j.nimb.2009.06.095

来源: Elsevier

【 摘 要 】

The laser-driven flyer system with a single pulses from a Q-switched Nd: glass laser, of 15 ns duration and up to 20 J energy, launched the aluminum films of 7 mu m thickness up to 8.3 km/s velocity in Beijing Institute of Spacecrafts Environment Engineering (BISEE) are briefly introduced. Some experimental aspects in our efforts on the space debris hypervelocity impacts on the outer surfaces functional of material, such as the thermal control material, window glass, OSR etc., are reviewed. Though still developing, the laser-driven flyer technique has been demonstrated promise in simulating micro M/OD hypervelocity impacting effects. (C) 2009 Elsevier B.V. All rights reserved.

【 授权许可】

Free