NASA Conference Publication, 3275. izdevums,3. daļaScientific and Technical Information Office, National Aeronautics and Space Administration., 1993 |
No grāmatas satura
1.–3. rezultāts no 66.
852. lappuse
... INTERACTIONS WITH MATERIALS III ( EOIM - III ) · An Overview of the Evaluation of Oxygen Interactions with Materials III Experiment : Space Shuttle Mission 46 , July August 1992 Steven L. Koontz , Lubert J. Leger , James T. Visentine ...
... INTERACTIONS WITH MATERIALS III ( EOIM - III ) · An Overview of the Evaluation of Oxygen Interactions with Materials III Experiment : Space Shuttle Mission 46 , July August 1992 Steven L. Koontz , Lubert J. Leger , James T. Visentine ...
903. lappuse
... Interactions with Materials III ( EOIM - III ) flight experiment was developed to obtain benchmark atomic oxygen / material reactivity data . The experiment was conducted during Space Shuttle mission 46 ( STS - 46 ) , which flew July 31 ...
... Interactions with Materials III ( EOIM - III ) flight experiment was developed to obtain benchmark atomic oxygen / material reactivity data . The experiment was conducted during Space Shuttle mission 46 ( STS - 46 ) , which flew July 31 ...
1096. lappuse
... interaction mechanisms of hyperthermal oxygen atoms with materials in LEO . The extent to which the laboratory results can lead to inferences about O- atom interactions in LEO depends on the ability of the laboratory experiment to ...
... interaction mechanisms of hyperthermal oxygen atoms with materials in LEO . The extent to which the laboratory results can lead to inferences about O- atom interactions in LEO depends on the ability of the laboratory experiment to ...
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