Computer optimization of spacecraft optical coatings for temperature control, using finite element analysis and matrix inversion
The selection of spacecraft optical coatings for temperature control.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE COMPUTER SYSTEMS CONFERENCE ; 1969 ; LOS ANGELES, CALIF.
01.09.1969
Aufsatz (Konferenz)
Keine Angabe
Englisch