28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
VERIFICATION OF OPTICAL PAYLOAD CFRP STRUCTURE FOR SATELLITE THROUGH ANALYSIS AND SPACE QUALIFICATION TEST
K. -J. Lee, H. -U. Oh, M. -S. Jo*, D. -J. Kim*
Agency for Defence Development, Korea; *Samsung Tales, Korea
Keywords: optical telescope, cfrp, structural analysis
Optical payload structure is designed with ultra-high modulus carbon fiber with cyanate resin with special stacking angle for optical and structural performance. Designed values of CFRP laminate and CFRP bonding structure are verified by analysis, coupon test and system qualification test.
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