NASA Conference Publication, 3275. izdevums,3. daļaScientific and Technical Information Office, National Aeronautics and Space Administration., 1993 |
No grāmatas satura
1.–3. rezultāts no 90.
939. lappuse
... exposure between the two AO exposure environments . Additionally , the EOIM III sample was exposed to a 25 % greater fluence than the ground - based LANL AO exposure sample , which could directly affect the amount of binder removed from ...
... exposure between the two AO exposure environments . Additionally , the EOIM III sample was exposed to a 25 % greater fluence than the ground - based LANL AO exposure sample , which could directly affect the amount of binder removed from ...
1003. lappuse
... exposure was demonstrated by passive exposure on STS - 41 as part of the ISAC experiment . The flight of EOIM - 3 provided the opportunity not only to expose and evaluate multiple specimens of black Kapton , but also to evaluate the ...
... exposure was demonstrated by passive exposure on STS - 41 as part of the ISAC experiment . The flight of EOIM - 3 provided the opportunity not only to expose and evaluate multiple specimens of black Kapton , but also to evaluate the ...
1026. lappuse
... exposure was during the EOIM - 3 part of the STS - 46 mission , when the Space Shuttle flew with the cargo bay oriented into the RAM direction at an altitude of 123-124 nautical miles . Additional atomic oxygen exposure of approximately ...
... exposure was during the EOIM - 3 part of the STS - 46 mission , when the Space Shuttle flew with the cargo bay oriented into the RAM direction at an altitude of 123-124 nautical miles . Additional atomic oxygen exposure of approximately ...
Saturs
Four Space Application Materials Coatings on the LongDuration | 854 |
Author Index | 857 |
Early Results from the Ultra Heavy Cosmic Ray Experiment 129 | 860 |
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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