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
Hauptverfasser: Elbakyan, Aram Tz, Balashov, Mikhael M., Filipenkov, Sergey N., Glazov, Gennady M., Gnoevaya, Nelly K., Kubar, Felix V., Sharipov, Rinat Kh
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container_issue
container_start_page 911
container_title SAE transactions
container_volume 103
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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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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