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Design for In-Flight Maintenance for Manned Space Missions
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English
Abstract
The reasons for and the design constraints associated with design for in-flight maintenance for manned space missions are discussed. Analytical techniques used to define problem areas and design experience derived from several current programs are presented. It is concluded that advantages of an in-flight maintainable system justifies the additional design effort required to achieve such a system.
Authors
Citation
Tillotson, R., "Design for In-Flight Maintenance for Manned Space Missions," SAE Technical Paper 640295, 1964, https://doi.org/10.4271/640295.Also In
References
- Tesch E. Plaisted R. Pukite J. “Control System Redundancy Mechanization Study.” 1962
- Pigg L. D. “Human Engineering Principles of Design for In-Space Maintenance.” Paper presented at Joint IAS-ARS Meeting Los Angeles June 1961
- Celentano J. T. Alexander H. S. “The Use of Tools in Space -- an Empirical Approach.” Paper presented at Joint IAS-ARS Meeting Los Angeles June 1961
- Bond N. A. “Maintaining Space Vehicles.” Paper presented at ARS Semi-Annual Meeting Los Angeles May 1960
- Grodsky M. A. “An Investigation of Crew Performance During a Seven-day Lunar Orbit Mission. Part I. Performance Results.” 1963