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Sapphire Viewports for a Venus ProbeA document discusses the creation of a viewport suitable for use on the surface of Venus. These viewports are rated for 500 C and 100 atm pressure with appropriate safety factors and reliability required for incorporation into a Venus Lander. Sapphire windows should easily withstand the chemical, pressure, and temperatures of the Venus surface. Novel fixture designs and seals appropriate to the environment are incorporated, as are materials compatible with exploration vessels. A test cell was fabricated, tested, and leak rate measured. The window features polish specification of the sides and corners, soft metal padding of the sapphire, and a metal C-ring seal. The system safety factor is greater than 2, and standard mechanical design theory was used to size the window, flange, and attachment bolts using available material property data. Maintenance involves simple cleaning of the window aperture surfaces. The only weakness of the system is its moderate rather than low leak rate for vacuum applications.
Document ID
20120016285
Acquisition Source
Goddard Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Bates, Stephen
(Thoughtventions Unltd. Glastonbury, CT, United States)
Date Acquired
August 26, 2013
Publication Date
October 1, 2012
Publication Information
Publication: NASA Tech Briefs, October 2012
Subject Category
Mechanical Engineering
Report/Patent Number
GSC-16095-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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