NASA Conference Publication, 3275. izdevums,3. daļa

absorptance active addition aluminum ambient analysis anodized Archive areas atomic oxygen attached beam calculated carbon cell Center coatings components composite contamination cover debris degradation detectors determined developed direct distribution Earth effects efficiency electron energy EOIM-III erosion Evaluation experiment exposed exposure Facility Figure flight flown fluence flux ground hardware heated impact increase indicated Interactions Kapton laboratory layer LDEF loss lubricant mass mass spectrometer materials measurements mirrors mission NASA O-atom observed obtained operations optical orbit oxide paint particle passive payload peak performed photographs plate polymer post-flight produced properties protection radiation reaction reactivity reflectance region requirements Research resistance samples scattering sensor showed shown in figure Shuttle significant silicon similar solar space environment Space Station spacecraft specimens spectra structure substrate surface System Table Teflon temperature thermal thermal control thickness tray vacuum values wavelength