Publication Date:
2019-07-13
Description:
Computer optimization of spacecraft optical coatings for temperature control, using finite element analysis and matrix inversion
Keywords:
THERMODYNAMICS AND COMBUSTION
Type:
AIAA PAPER 69-979
,
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE COMPUTER SYSTEMS CONFERENCE; Sep 08, 1969 - Sep 10, 1969; LOS ANGELES, CA|; 5-10 (
Format:
text
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