Transit Thermal Control Design for Galileo Entry Probe for Planet Jupiter

George C. Haverly; William Pitts

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NASA NTRS · 19820017418

Transit Thermal Control Design for Galileo Entry Probe for Planet Jupiter

George C. Haverly·William Pitts

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Abstract

A totally passive design was completed for the thermal control of the Galileo entry probe during its transit to the planet Jupiter. The design utilizes radio isotope heater units, multilayer insulation blankets and a thermal radiator in conjunction with a design conductance support structure to achieve both the required storage and critical initial planet atmosphere entry temperatures. The probe transit thermal design was completed and verified based on thermal vacuum testing of a prototype probe thermal test model.

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George C. Haverly, William Pitts. 1982-05-17. Transit Thermal Control Design for Galileo Entry Probe for Planet Jupiter. https://ntrs.nasa.gov/citations/19820017418

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