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PIUME: In space as on earth, on earth as in space 

Cecchini, Gabriele; Lobascio, Cesare; Vidal-Peir�, Pau (50th International Conference on Environmental Systems, 7/12/2021)
When humans live and work in extreme conditions, vital resource must be managed with extreme care. International Space Station (ISS) today, Moon and Mars surface outposts tomorrow provide an inspiring approach for new ...
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Lithium Chloride Absorber Radiator for Mars Exploration 

Izenson, Michael; Phillips, Scott; Deserranno, Dimitri; Chepko, Ariane (47th International Conference on Environmental Systems, 2017-07-16)
Life support systems for Mars exploration space suits will face challenging requirements for heat rejection. These systems must be light weight, compact, rugged, make minimal use of consumables, and have low impact on the ...
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A comparison study on thermal control techniques for a nanosatellite carrying infrared science instrument 

Selvadurai, Shanmugasundaram; Chandran, Amal; Valentini, David; Edwin, Teo Hang Tong; Chandrakant Joshi, Sunil; Olschewski, Friedhelm (2020 International Conference on Environmental Systems, 2020-07-31)
Based on current technological advancements and forecasts, nanosatellites will be used for both scientific and defense applications leveraging advantages on both development cost and development lifecycle. As nanosatellites ...
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Development and Testing of Re-Deployable Radiator for Deep Space Exploration Technology Demonstrator, DESTINY+ 

Akizuki, Yuki; Nagano, Hosei; Kinjo, Tomihiro; Sawada, Kenichiro; Ogawa, Hiroyuki; Takashima, Takeshi; Nishiyama, Kazutaka; Toyota, Hiroyuki; Watanabe, Kazuki; Kuratomi, Takeshi (49th International Conference on Environmental Systems, 2019-07-07)
A Reversible Thermal Panel (RTP) is a flexible re-deployable radiator that autonomously controls the temperature of a heat source. It promotes heat dissipation by deploying the radiator surface when the heat source is at ...
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Interdisciplinary Development of the METimage Cryogenic Sub-System Thermo-Mechanical Design 

Schweikle, Robert; Hauser, Armin; Buhl, Nadine; Naire, Raphael (2020 International Conference on Environmental Systems, 2020-07-31)
METimage is a multispectral imaging optical instrument with a wide coverage realized by a scanning design. It is part of the instrument suite on satellite-type A of the Metrological Operational Satellite –Second Generation ...
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Development of Lithium Chloride Absorber Radiator for Flight Demonstration 

Izenson, Michael; Phillips, Scott; Chepko, Ariane; Daines, Gregory; Quinn, Gregory; Steele, John (47th International Conference on Environmental Systems, 2017-07-16)
Water conservation is an essential requirement for future exploration space suits. Lithium Chloride Absorber Radiator (LCAR) technology has been developed to meet this requirement by rejecting heat without venting water ...
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Phase Change Material Heat Accumulator for the HEXAFLY Hypersonic Glider 

Collette, Jean-Paul; Rochus, Pierre; Steelant, Johan; Peyrou-Lauga, Romain; Nutal, Nicolas; Andro, Jean-Yves; Nadalini, Riccardo; Romero Fernandez, Pedro (49th International Conference on Environmental Systems, 2019-07-07)
From the launchers to the spacecrafts, various on-board systems have to be maintained within specified temperature limits. Phase Change Materials (PCM) offer the possibility to store thermal energy directly as latent heat ...
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Design and Flight Performance of the Combined Thermal Control System of the BOLIDE Experiment in Balloon Mission PMC Turbo/2018 

Baturkin, Volodymyr; Kaifler, Bernd; Rempel, Dimitry; Kaifler, Natalie; Spröwitz, Tom; Henning, Fabian; Roßi, Philipp (2020 International Conference on Environmental Systems, 2020-07-31)
The Polar Mesospheric Cloud Turbulence experiment (PMC Turbo) is intended to observe and quantify the dynamics of small-scale gravity waves and instabilities in the upper mesosphere. The instruments aboard a stratospheric ...
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A Variable-View-Factor Two-Phase Radiator Manufactured Via Ultrasonic Welding 

Diebold, Jeff; Tarau, Calin; Lutz, Andy; Rokkam, Srujan; Eff, Michael; Lindamood, Lindsey (50th International Conference on Environmental Systems, 7/12/2021)
Radiators for manned spacecraft, satellites, planetary rovers and unmanned spacecraft are typically sized for the highest power at the hottest sink conditions, so they are oversized and prone to freezing at low sink ...
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Development of Variable Emissivity Coating for Thermal Radiator 

Dudon, Jean-Paul; Dubost, Laurent; Remaury, Stephanie; Marcel, Corinne; Ravaux, Alice; Aubert, Pierre-Henri; Duzellier, Sophie; Divay, Laurent (50th International Conference on Environmental Systems, 7/12/2021)
For years the use of variable emissivity devices and coatings has been envisaged by the academic and industrials space actors. The aim is to overcome the drawback specific to constant thermo-optical coatings with regard ...
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AuthorPeyrou-Lauga, Romain (4)Nagano, Hosei (3)Chepko, Ariane (2)Izenson, Michael (2)Persson, Jan (2)Phillips, Scott (2)Akin, David (1)Akizuki, Yuki (1)Andro, Jean-Yves (1)Aubert, Pierre-Henri (1)... View MoreSubject
Thermal control (25)
Spacecraft (4)Radiator (3)International Space Station (2)Phase Change Material (2)Thermal straps (2)Additive manufacturing (1)Airbus (1)Analog field trials (1)Autonomy (1)... View MoreDate Issued2020 (7)2021 (6)2019 (5)2017 (3)2016 (2)2018 (2)Has File(s)Yes (25)

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