From Concept to Flight: An Active Fluid Loop Based Thermal Control System for Mars Science Laboratory Rover

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From Concept to Flight: An Active Fluid Loop Based Thermal Control System for Mars Science Laboratory Rover

Birur, G. / Bhandari, P. / Bame, D. / Karlmann, P. / Mastropietro, A. / Liu, Y. / Miller, J. / Pauken, M. / Lyra, J. / American Institute of Aeronautics and Astronautics

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Dokumentinformationen

Titel :

From Concept to Flight: An Active Fluid Loop Based Thermal Control System for Mars Science Laboratory Rover

Beteiligte:

Birur, G. (Autor:in) / Bhandari, P. (Autor:in) / Bame, D. (Autor:in) / Karlmann, P. (Autor:in) / Mastropietro, A. (Autor:in) / Liu, Y. (Autor:in) / Miller, J. (Autor:in) / Pauken, M. (Autor:in) / Lyra, J. (Autor:in) / American Institute of Aeronautics and Astronautics

Kongress:

International conference; 42nd, Environmental systems ; 2012 ; San Diego, CA

Erschienen in:

Environmental systems ; 1352-1361

PAPERS- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; 2

Erscheinungsdatum :

2012-01-01

Format / Umfang :

10 pages

Anmerkungen:

Includes bibliographical references and index; Also known as ICES 2012

ISBN :