contributor author | N. C. Willis | |
contributor author | F. H. Samonski | |
contributor author | Charles Flugel | |
contributor author | Paul Tremblay | |
date accessioned | 2017-05-09T01:03:18Z | |
date available | 2017-05-09T01:03:18Z | |
date copyright | November, 1971 | |
date issued | 1971 | |
identifier issn | 1087-1357 | |
identifier other | JMSEFK-27566#1145_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/153377 | |
description abstract | The preliminary design phase of the Space Station Prototype Environmental Thermal Control and Life Support System Program has been completed, and the detailed design of the system is underway. This paper describes some of the specific system features which have been incorporated to solve the problems of maintainability, to ensure reliability without excessive weight penalties, and to achieve fault detection and isolation through use of the capabilities of an onboard checkout system. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | System Features of a Space Station Prototype Environmental Thermal Control and Life Support System | |
type | Journal Paper | |
journal volume | 93 | |
journal issue | 4 | |
journal title | Journal of Manufacturing Science and Engineering | |
identifier doi | 10.1115/1.3428054 | |
journal fristpage | 1145 | |
journal lastpage | 1151 | |
identifier eissn | 1528-8935 | |
keywords | Engineering prototypes | |
keywords | Space stations | |
keywords | Design | |
keywords | Flaw detection | |
keywords | Maintainability | |
keywords | Weight (Mass) AND Reliability | |
tree | Journal of Manufacturing Science and Engineering:;1971:;volume( 093 ):;issue: 004 | |
contenttype | Fulltext | |