Structure stability of precision component made of carbon fiber composite in space optical remote sensor

LI Wei; LIU Hong-wei

Optics and Precision Engineering, Volume. 16, Issue 11, 2173(2008)

LI Wei^* and LIU Hong-wei

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[in Chinese]

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References(4)

[7] [7] SEUMM J E,PHNCHON G E.Graphite/epoxy material characteristics and design techniques for airborne instrument application[J].SPIE,1982,309:188-198

[8] [8] CCONNELL S J,DODSOM K J,FRIEDMAN Z,et al..Design progression of an all-composite primary mirror for the FIRST telescope[J].SPIE,2000,4013:173-183

[10] [10] CONNELL S J,ABUSAFIEH A.Lightweight space mirrors from carbon fiber composites[J].SAMPE Journal,2002,38(4):46-55

[11] [11] ROBERT C R.CFRP composites for optics and structures in telescope applications[J].SPIE,2543:154-161

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LI Wei, LIU Hong-wei. Structure stability of precision component made of carbon fiber composite in space optical remote sensor[J]. Optics and Precision Engineering, 2008, 16(11): 2173

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Paper Information

Category:

Received: Aug. 6, 2008

Accepted: --

Published Online: Feb. 28, 2010

The Author Email: LI Wei (leew2006@ciomp.ac.cn)

DOI:

CSTR:32186.14.

Topics

laser devices and laser physics

Lasers and Laser Optics

Laser physics

laser manufacturing

Instrumentation, Measurement and Metrology