Demonstration of a Plug-And-Play Approach to Spacecraft Thermal Control System Design

The thermal demands placed on interplanetary probes and rovers can vary wildly throughout the course of a given mission. As the electronics and other equipment on these rovers become more sophisticated, heat dissipation and thermal control become more of an issue. Further complicating the thermal co...

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Bibliographische Detailangaben

Hauptverfasser:	Maxwell, Eric B, Cole, Gregory S, Scaringe, Robert P, Didion, Jeffrey
Format:	Tagungsbericht
Sprache:	eng
Online-Zugang:	Volltext
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