NASA Technical Reports Server
+ Visit NASA.gov
+ Contact NASA
ABOUT NTRS SEARCH NTRS NTRS NEWS HELP FEEDBACK ORDER NASA INFO.
  + Home
SEARCH NTRS
Navigattion Search Options
Collection > NASA 

Author > Gaier, James R. 
Author > Larkin, Elizabeth M. G. 
Author > Panko, Scott R. 
Author > Rogers, Kerry J. 
Author > Siamidis, John 

NASA Center > Glenn Research Center 

Publication Year > 2001-2010 > 2008 

Subject > J-L > Lunar And Planetary Science And Exploration 

Availability Options > Order From CASI > CD-ROM, DVD, Print 

Item/Media Type > NASA Report > Technical Memorandum (TM) 
Item/Media Type > Technical Report 


Note: Start a new navigation search by selecting a link above

Image of Earth and the Proteus research aircraft with spiral galaxy in background and the words 'Aerospace Information for a Changing World' Visit the STI Program Web Site
SEARCH NTRS

    Previous Record | Next Record + Back to Results

  + Printer Friendly
Title: The Effect of Simulated Lunar Dust on the Absorptivity, Emissivity, and Operating Temperature on AZ-93 and Ag/FEP Thermal Control Surfaces
Author(s): Gaier, James R.; Siamidis, John; Panko, Scott R.; Rogers, Kerry J.; Larkin, Elizabeth M. G.
Abstract: JSC-1AF lunar simulant has been applied to AZ-93 and AgFEP thermal control surfaces on aluminum or composite substrates in a simulated lunar environment. The temperature of these surfaces was monitored as they were heated with a solar simulator and cooled in a 30 K coldbox. Thermal modeling was used to determine the absorptivity ( ) and emissivity ( ) of the thermal control surfaces in both their clean and dusted states. Then, a known amount of power was applied to the samples while in the coldbox and the steady state temperatures measured. It was found that even a submonolayer of simulated lunar dust can significantly degrade the performance of both white paint and second-surface mirror type thermal control surfaces under these conditions. Contrary to earlier studies, dust was found to affect as well as . Dust lowered the emissivity by as much as 16 percent in the case of AZ-93, and raised it by as much as 11 percent in the case of AgFEP. The degradation of thermal control surface by dust as measured by / rose linearly regardless of the thermal control coating or substrate, and extrapolated to degradation by a factor 3 at full coverage by dust. Submonolayer coatings of dust were found to not significantly change the steady state temperature at which a shadowed thermal control surface will radiate.
NASA Center: Glenn Research Center
Publication Date: December 2008
Document Source: CASI
No Digital Version Available: Go to Tips On Ordering
Document ID: 20090005996
Publication Information: Number of Pages = 21
Report Number: E-16723; NASA/TM-2008-215492
Contract-Grant-Task Number: WBS 936374.04.08.03
Price Code: A03
Keywords: LUNAR DUST; LUNAR ENVIRONMENT; LUNAR SOIL; ABSORPTIVITY; EMISSIVITY; OPERATING TEMPERATURE; THERMAL CONTROL COATINGS; CONTROL SURFACES; STEADY STATE; DEGRADATION; SUBSTRATES;
Accessibility: Unclassified; Copyright; Unlimited; Publicly available;
Updated/Added to NTRS: 2009-02-11

+ Back to Top

USAGov logoExternal Site
+ Sponsored by the NASA Scientific and Technical
   Information Program

+ 2004 Vision for Space Exploration
+ Freedom of Information Act
+ NASA Web Privacy Policy and Important Notices
+ NASA Disclaimers, Copyright Notice,
   and Terms and Conditions of Use


NASA

NASA Official: Calvin Mackey
Page Curator: NASA Center for AeroSpace Information (help@sti.nasa.gov)
Last Updated: July 5, 2007