The analysis for determining the optimum cylindrical length of the Space Station Freedom (SSF) Pressurized Logistics Module, whose task is to transport the SSF pressurized cargo via the NSTS Shuttle Orbiter, is described. The major factors considered include the NSTS net launch lift capability, the pressurized cargo requirements, and the mass properties of the module structures, mechanisms, and subsystems.
Optimization of the Pressurized Logistics Module - A Space Station Freedom analytical study
1991-11-01
Conference paper
No indication
English
Mini-pressurized logistics module for Space Station Freedom
Online Contents | 1994
|Mini-pressurized logistics module for Space Station Freedom
British Library Conference Proceedings | 1994
|Pressurized modules for Space Station Freedom
NTRS | 1993
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