DocumentCode
3514758
Title
Extreme Temperature Sensing System for Venus Surface Missions
Author
Del Castillo, Linda ; West, William ; Vo, Tuan ; Hatake, Toshiro ; Mojarradi, Mohammad ; Kolawa, Elizabeth
Author_Institution
Jet Propulsion Lab., Pasadena, CA
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
6
Abstract
Previous Venus landers used high temperature pressure vessels with passive thermal protection systems and protected conventional electronics, which limited their surface operation life to 127 minutes. The operating life and science return for future Venus surface missions, however, can significantly be increased through the use of high temperature electronics capable of extending the operating range of electronic systems to Venus surface temperatures (up to 480degC). Toward that end, this paper details the development and evaluation (at 480degC) of a stand-alone, high temperature, battery powered, sensor system, including a multi-sensor interface, multiplexer, signal conditioner, and amplifier, that can directly operate at the extremely high temperatures of the Venus surface. This work employs commercial, high temperature sensors, electronic devices, and packaging materials and leverages their operating margin to realize the aforementioned high temperature sensor system. As a result, the technology could rapidly rise through technology readiness level gates for future NASA missions to Venus.
Keywords
Venus; aerospace instrumentation; high-temperature electronics; instrument landing systems; temperature measurement; temperature sensors; Venus landers; Venus surface missions; extreme temperature sensing system; high temperature electronics; Batteries; Electronics packaging; High power amplifiers; Multiplexing; Protection; Sensor systems; Space technology; Temperature distribution; Temperature sensors; Venus;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526492
Filename
4526492
Link To Document