186. Space Vehicle Weight and Performance Optimization

Title186. Space Vehicle Weight and Performance Optimization
Publication TypeConference Paper
Paper Number0186
Year of Publication1958
AuthorsRiley, F.
Conference17th Annual Conference, Belmont Plaza Hotel, New York, New York, May 19-22
Conference LocationNew York, New York
PublisherSociety of Allied Weight Engineers, Inc.
Date Published5/19/58
Abstract

A summary method of correlating performance and weight parameters to yield an optimum missile design is discussed. A specific end use is selected to demonstrate the summary method described.

Accepting the premise: “Minimum weight requirements shall take precedence over ease of maintenance, easy and rapid installation of propulsion group and accessories and ease of installation”, a summary method of determining optimum weight is deve1oed to satisfy the basic design criteria.

Pages26
Key Words19. Weight Engineering - Spacecraft Estimation
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