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Accession Number:
AD0612016
Title:
PROGRAM ROE (REFLECTOR ORBITAL EXPERIMENT). PART III. PRELIMINARY DESIGN: INFLATABLE RIGIDIZED SOLAR REFLECTOR CONCEPT. VOLUME II. PARAMETRIC DESIGN STUDY OF INFLATABLE SOLAR REFLECTOR THERMAL DEFLECTIONS.
Corporate Author:
LOCKHEED MISSILES AND SPACE CO SUNNYVALE CALIF
Report Date:
1964-12-01
Abstract:
A computer program was developed for analysis of contour deviations as a function of the thermal environment and the physical properties of materials used in solar concentrators of an inflatable rigidizable construction. The program was applied to a study of the effects of changing various design parameters such as surface thermal properties, core density and concentrator dimensions. The detail effort consisted of establishing a digital computer program suitable for the IBM Model 7094 Fortran II Language. Instructions for use of this program are presented. Two complete source decks have been delivered to the Air Force Aero Propulsion Laboratory. Author
Supplementary Note:
See also Volume 1, AD-612 460 and Part 1, AD-612 014.
Pages:
0274
Contract Number:
AF 33(657)-10668
File Size:
0.00MB
