NASA Conference Publication, 3275. izdevums,3. daļaScientific and Technical Information Office, National Aeronautics and Space Administration., 1993 |
No grāmatas satura
1.–3. rezultāts no 59.
1023. lappuse
... Wavelength ( nm ) Control a = 0 938 →→ Exposed a = 0 959 8 Exposed Central Figure 11. EOIM - 3 Viton integrated reflectance as a function of wavelength . Figure 13. FTIR of EOIM - 3 exposed Viton showing percent transmission as a ...
... Wavelength ( nm ) Control a = 0 938 →→ Exposed a = 0 959 8 Exposed Central Figure 11. EOIM - 3 Viton integrated reflectance as a function of wavelength . Figure 13. FTIR of EOIM - 3 exposed Viton showing percent transmission as a ...
1049. lappuse
... wavelength range includes wavelengths at which the incident energy from the sun has the highest potential to induce rupture of chemical bonds.9 It is not clear from the data available why the 2219 substrate degraded more than the 7075 ...
... wavelength range includes wavelengths at which the incident energy from the sun has the highest potential to induce rupture of chemical bonds.9 It is not clear from the data available why the 2219 substrate degraded more than the 7075 ...
1185. lappuse
... wavelengths beyond 250 μm , the short wavelength spectra could be reproduced and the interference fringes could be roughly reproduced without allowing the dielectric properties to vary with wavelength . The results suggest that the ...
... wavelengths beyond 250 μm , the short wavelength spectra could be reproduced and the interference fringes could be roughly reproduced without allowing the dielectric properties to vary with wavelength . The results suggest that the ...
Saturs
Author Index | 857 |
Early Results from the Ultra Heavy Cosmic Ray Experiment 129 | 860 |
Image and Compositional Characteristics of the Big Guy LDEF | 863 |
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Aerospace ambient analysis anodized Archive System atomic oxygen atomic oxygen exposure atomic oxygen fluence atoms/cm² attached payload beam beta cloth binder carbon Center composite contamination control sample database debris degradation detectors effects electron EOIM EOIM-III erosion Evaluation exposed F-center flight experiments flight sample flown fluence flux graphite hardware heated trays impact indicated Kapton laboratory LANL layer LDEF LDEF Archive Long Duration Exposure low earth orbit mass spectrometer measurements meteoroid mirrors mission MSFC NASA O-atom optical density optical properties outgassing oxide Oxygen Interactions paint Pallet particle passive tray polyimide polymer post-flight Post-Retrieval Symposium pre-flight radiation reaction efficiency reactivity reflectance sensor showed shown in figure silicon solar absorptance solar cell space environment space exposure Space Shuttle Space Station spacecraft specimens spectra substrate surface Table Teflon temperature thermal control coatings thickness thin film ultraviolet unexposed vacuum Viton wavelength X-ray photoelectron spectroscopy