The Automatic Thermal Control System (ATCS) for the EVA Space Suit
This paper presents some approaches to implementation of an automatic thermal control system for the manned space suit. Both the investigation of the space suit thermal conditions performed by ZVEZDA and analysis of these conditions during cosmonauts activities at SALUTE-6, SALUTE-7 and MIR space st...
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Veröffentlicht in: | SAE transactions 1994-01, Vol.103, p.911-923 |
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creator | Elbakyan, Aram Tz Balashov, Mikhael M. Filipenkov, Sergey N. Glazov, Gennady M. Gnoevaya, Nelly K. Kubar, Felix V. Sharipov, Rinat Kh |
description | This paper presents some approaches to implementation of an automatic thermal control system for the manned space suit. Both the investigation of the space suit thermal conditions performed by ZVEZDA and analysis of these conditions during cosmonauts activities at SALUTE-6, SALUTE-7 and MIR space stations have provided a great body of information for ATCS implementation. The paper presents the experimental data on one modification of operating ORLAN-type space suit ATCS model. |
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Both the investigation of the space suit thermal conditions performed by ZVEZDA and analysis of these conditions during cosmonauts activities at SALUTE-6, SALUTE-7 and MIR space stations have provided a great body of information for ATCS implementation. The paper presents the experimental data on one modification of operating ORLAN-type space suit ATCS model.</description><subject>Astronauts</subject><subject>Control systems</subject><subject>Cooling</subject><subject>Extravehicular activity</subject><subject>Inlets</subject><subject>Liquid cooling</subject><subject>Skin temperature</subject><subject>Space suits</subject><subject>Water temperature</subject><issn>0096-736X</issn><issn>2577-1531</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1994</creationdate><recordtype>article</recordtype><sourceid/><recordid>eNqFir0KgzAYAENpofbnEQrf2A5CYtTgaMXSPSLdJEikimkk-Rx8-zp073QcdxsSRIkQIUs425KA0iwNBU9fe3LwfqCUs0REAblXbw35jNYo7FtYzRk1QmE_6OwIcvGoDVzzqpA36KwDXP-yzkFOqtUg5x5PZNep0evzj0dyeZRV8QwHj9Y1k-uNcksTxymLMyr4v_4FJxo03w</recordid><startdate>19940101</startdate><enddate>19940101</enddate><creator>Elbakyan, Aram Tz</creator><creator>Balashov, Mikhael M.</creator><creator>Filipenkov, Sergey N.</creator><creator>Glazov, Gennady M.</creator><creator>Gnoevaya, Nelly K.</creator><creator>Kubar, Felix V.</creator><creator>Sharipov, Rinat Kh</creator><general>Society of Automotive Engineers, Inc</general><scope/></search><sort><creationdate>19940101</creationdate><title>The Automatic Thermal Control System (ATCS) for the EVA Space Suit</title><author>Elbakyan, Aram Tz ; Balashov, Mikhael M. ; Filipenkov, Sergey N. ; Glazov, Gennady M. ; Gnoevaya, Nelly K. ; Kubar, Felix V. ; Sharipov, Rinat Kh</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-jstor_primary_446149073</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1994</creationdate><topic>Astronauts</topic><topic>Control systems</topic><topic>Cooling</topic><topic>Extravehicular activity</topic><topic>Inlets</topic><topic>Liquid cooling</topic><topic>Skin temperature</topic><topic>Space suits</topic><topic>Water temperature</topic><toplevel>online_resources</toplevel><creatorcontrib>Elbakyan, Aram Tz</creatorcontrib><creatorcontrib>Balashov, Mikhael M.</creatorcontrib><creatorcontrib>Filipenkov, Sergey N.</creatorcontrib><creatorcontrib>Glazov, Gennady M.</creatorcontrib><creatorcontrib>Gnoevaya, Nelly K.</creatorcontrib><creatorcontrib>Kubar, Felix V.</creatorcontrib><creatorcontrib>Sharipov, Rinat Kh</creatorcontrib><jtitle>SAE transactions</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Elbakyan, Aram Tz</au><au>Balashov, Mikhael M.</au><au>Filipenkov, Sergey N.</au><au>Glazov, Gennady M.</au><au>Gnoevaya, Nelly K.</au><au>Kubar, Felix V.</au><au>Sharipov, Rinat Kh</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>The Automatic Thermal Control System (ATCS) for the EVA Space Suit</atitle><jtitle>SAE transactions</jtitle><date>1994-01-01</date><risdate>1994</risdate><volume>103</volume><spage>911</spage><epage>923</epage><pages>911-923</pages><issn>0096-736X</issn><eissn>2577-1531</eissn><abstract>This paper presents some approaches to implementation of an automatic thermal control system for the manned space suit. Both the investigation of the space suit thermal conditions performed by ZVEZDA and analysis of these conditions during cosmonauts activities at SALUTE-6, SALUTE-7 and MIR space stations have provided a great body of information for ATCS implementation. The paper presents the experimental data on one modification of operating ORLAN-type space suit ATCS model.</abstract><pub>Society of Automotive Engineers, Inc</pub></addata></record> |
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ispartof | SAE transactions, 1994-01, Vol.103, p.911-923 |
issn | 0096-736X 2577-1531 |
language | eng |
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source | JSTOR Archive Collection A-Z Listing |
subjects | Astronauts Control systems Cooling Extravehicular activity Inlets Liquid cooling Skin temperature Space suits Water temperature |
title | The Automatic Thermal Control System (ATCS) for the EVA Space Suit |
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