A hypervelocity debris simulating technique with laser driven flyer

Tong Jingyu; Huang Bencheng; Pang Hewei; Dong Hongjian; Wang Jihui

A hypervelocity debris simulating technique with laser driven flyer

Tong Jingyu, Huang Bencheng, Pang Hewei, Dong Hongjian, Wang Jihui

Beijing Institute of Satellite Environment Engineering

Research output: Contribution to journal › Conference article › peer-review

Abstract

This paper describes a relatively new method to simulate space debris by the laser driven flyer technique. A neodymium-glass pulsed laser was used in this work, capable of up 20 joules in 20 nanoseconds. A 2mm diameter, 66micron thick aluminum flyer was accelerated to 3km/s with the technique. The hypervelocity impact test on some space materials has been completed at Beijing Institute of Satellite Environment Engineering. It is successful to conduct an initial investigation of impact damage for thermal control paints and graphite/epoxy composite.

Original language	English
Pages (from-to)	951-955
Number of pages	5
Journal	Advances in the Astronautical Sciences
Volume	117
Publication status	Published - 2004
Externally published	Yes
Event	10th International Conference of Pacific Basin Societies, ISCOPS - Tokyo, Japan Duration: 10 Dec 2003 → 12 Dec 2003

Cite this

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title = "A hypervelocity debris simulating technique with laser driven flyer",

abstract = "This paper describes a relatively new method to simulate space debris by the laser driven flyer technique. A neodymium-glass pulsed laser was used in this work, capable of up 20 joules in 20 nanoseconds. A 2mm diameter, 66micron thick aluminum flyer was accelerated to 3km/s with the technique. The hypervelocity impact test on some space materials has been completed at Beijing Institute of Satellite Environment Engineering. It is successful to conduct an initial investigation of impact damage for thermal control paints and graphite/epoxy composite.",

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journal = "Advances in the Astronautical Sciences",

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note = "10th International Conference of Pacific Basin Societies, ISCOPS ; Conference date: 10-12-2003 Through 12-12-2003",

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AU - Jingyu, Tong

AU - Bencheng, Huang

AU - Hewei, Pang

AU - Hongjian, Dong

AU - Jihui, Wang

PY - 2004

Y1 - 2004

N2 - This paper describes a relatively new method to simulate space debris by the laser driven flyer technique. A neodymium-glass pulsed laser was used in this work, capable of up 20 joules in 20 nanoseconds. A 2mm diameter, 66micron thick aluminum flyer was accelerated to 3km/s with the technique. The hypervelocity impact test on some space materials has been completed at Beijing Institute of Satellite Environment Engineering. It is successful to conduct an initial investigation of impact damage for thermal control paints and graphite/epoxy composite.

AB - This paper describes a relatively new method to simulate space debris by the laser driven flyer technique. A neodymium-glass pulsed laser was used in this work, capable of up 20 joules in 20 nanoseconds. A 2mm diameter, 66micron thick aluminum flyer was accelerated to 3km/s with the technique. The hypervelocity impact test on some space materials has been completed at Beijing Institute of Satellite Environment Engineering. It is successful to conduct an initial investigation of impact damage for thermal control paints and graphite/epoxy composite.

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M3 - Conference article

AN - SCOPUS:23744475395

SN - 0065-3438

VL - 117

SP - 951

EP - 955

JO - Advances in the Astronautical Sciences

JF - Advances in the Astronautical Sciences

T2 - 10th International Conference of Pacific Basin Societies, ISCOPS

Y2 - 10 December 2003 through 12 December 2003

ER -

A hypervelocity debris simulating technique with laser driven flyer

Abstract

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