Integrated Thermal Simulation of the Space Evaporator Absorber Radiator using TherMoS and V-SUIT

dc.creatorGierszewski, Daniel
dc.creatorOlthoff, Claas
dc.date.accessioned2016-07-28T19:19:44Z
dc.date.available2016-07-28T19:19:44Z
dc.date.issued2016-07-10
dc.descriptionGermany
dc.descriptionTechnical University of Munich, Institute of Astronautics
dc.descriptionTechnical University of Munich
dc.description402
dc.descriptionICES402: Extravehicular Activity: PLSS Systems
dc.descriptionVienna, Austria
dc.descriptionDaniel Gierszewski, Technical University of Munich, Germany
dc.descriptionThe 46th International Conference on Environmental Systems was held in Vienna, Austria, USA on 10 July 2016 through 14 July 2016.
dc.descriptionClaas T. Olthoff, Technical University of Munich, Germany
dc.description.abstractThe Space Evaporator Absorber Radiator (SEAR) developed by Creare LLC and NASA is a novel technology for thermal control of spacesuits. It greatly reduces the amount of water lost through evaporative cooling by absorbing it into a lithium chloride bed. This process generates heat that needs to be radiated away from the spacesuit in order to maintain acceptable absorption rates. In contrast to the operation of current spacesuits, this creates a dependency between the spacesuit cooling system and the thermal environment in which the suit operates. In order to asses this dependency and the effect the thermal environment would have on this system, two dynamic simulation tools have been developed at the Technical University of Munich in the past years: The Thermal Moon Simulator (TherMoS) and the dynamic portable life support system (PLSS) simulation Virtual Space Suit (V‑SUIT). Both tools are MATLAB®-based and spin-offs from the Virtual Habitat (V‑HAB) project. V-SUIT can dynamically simulate space suit portable life support systems and their interaction with a detailed and dynamic human model. TherMoS provides information about the heat transfer between the space suit and its environment. To achieve this, a detailed thermal model of the lunar surface is created including three-dimensional features like craters and boulders. This paper describes the modeling of SEAR in V‑SUIT and TherMoS. Integrated thermal simulations of several scenarios with different thermal environments and different crew member metabolic rates were performed. Results show the interrelations between SEAR performance, the metabolic rate and the dynamic thermal environment. Even though water loss through a vent valve in case of excessive heat load cannot be completely prevented, the simulation results suggest a great potential for water savings when using SEAR.
dc.format.mimetypeapplication/pdf
dc.identifier.otherICES_2016_289
dc.identifier.urihttp://hdl.handle.net/2346/67646
dc.language.isoeng
dc.publisher46th International Conference on Environmental Systems
dc.subjectDynamic Simulations
dc.subjectIntegrated Thermal Simulations
dc.subjectSpace Suit Cooling Systems
dc.subjectSEAR
dc.subjectV-SUIT
dc.titleIntegrated Thermal Simulation of the Space Evaporator Absorber Radiator using TherMoS and V-SUIT
dc.typePresentation

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