Proceedings Paper
Design and producibility of precision beryllium structures for spacecraft applications| Format | Member Price | Non-Member Price |
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Paper Abstract
Basic design guidelines for beryllium precision structures are discussed and a thorough presentation is given on the design evolution of the RGA integrating structure for ESA's XMM Mission. Beryllium producibility issues, manufacturing flowcharts and flight heritage data is reviewed.
Paper Details
Date Published: 23 October 1995
PDF: 23 pages
Proc. SPIE 2543, Silicon Carbide Materials for Optics and Precision Structures, (23 October 1995); doi: 10.1117/12.225282
Published in SPIE Proceedings Vol. 2543:
Silicon Carbide Materials for Optics and Precision Structures
Mark A. Ealey, Editor(s)
PDF: 23 pages
Proc. SPIE 2543, Silicon Carbide Materials for Optics and Precision Structures, (23 October 1995); doi: 10.1117/12.225282
Show Author Affiliations
Robert E. Hardesty, The Peregrine Falcon Corp. (United States)
Todd A. Decker, Lawrence Livermore National Lab. (United States)
Published in SPIE Proceedings Vol. 2543:
Silicon Carbide Materials for Optics and Precision Structures
Mark A. Ealey, Editor(s)
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