During this reporting period, the phase 1 interim report was written and submitted. Detailed computer models were used to predict exposure to atomic oxygen and solar ultraviolet radiation. ESCA survey measurements were started on the tray wall section cut from LDEF tray location EIO-3. At this time there are no technical issues impeding the progress of the required tasks. Cost are in line withn the percentage of completion of tasks. The expended budget is 18% of the total and the project is approximately 18% complete. During the next reporting period we will continue to analyze points from tray locations E10-3 and A4-1 using ESCA and auger surface analysis techniques and a detailed location map will be produced
The atomic oxygen flux exposure experiments flown on Space Shuttle flights STS-5 and STS-8 are descr...
Thermal control coatings within the recessed compartments of LDEF Experiment A0034 experienced the m...
Contamination that leads to degradation of critical surfaces becomes a vital design issue for many s...
Electron Spectroscopy for Chemical Analysis (ESCA) survey measurements completed on the tray wall se...
Contaminant deposition measurements have been made on species content and depth profiles on three ex...
A computer model for prediction of atomic oxygen exposure of spacecraft in low earth orbit, referred...
Computer models of environmental conditions in Earth orbit are needed for the following reasons: (1)...
Atomic oxygen exposures were determined analytically for rows, longerons, and end bays of the Long D...
Atomic oxygen (AO) fluences and solar exposure have been modeled for selected hardware from the Long...
One of the primary causes of material degradation in low Earth orbit (LEO) is exposure to atomic oxy...
In the flight materials exposure data base extensive quantitative data is available from limited exp...
The LDEF mission was to study the effects of the space environment on various materials over an exte...
The Evaluation of Oxygen Interactions with Materials 3 (EOIM-3) flight experiment was developed to o...
The definition of LDEF atomic oxygen exposure involves theoretical prediction of fluxes, modeling of...
Power degradation in the solar cells was consistent with the exposure environment and appears to be ...
The atomic oxygen flux exposure experiments flown on Space Shuttle flights STS-5 and STS-8 are descr...
Thermal control coatings within the recessed compartments of LDEF Experiment A0034 experienced the m...
Contamination that leads to degradation of critical surfaces becomes a vital design issue for many s...
Electron Spectroscopy for Chemical Analysis (ESCA) survey measurements completed on the tray wall se...
Contaminant deposition measurements have been made on species content and depth profiles on three ex...
A computer model for prediction of atomic oxygen exposure of spacecraft in low earth orbit, referred...
Computer models of environmental conditions in Earth orbit are needed for the following reasons: (1)...
Atomic oxygen exposures were determined analytically for rows, longerons, and end bays of the Long D...
Atomic oxygen (AO) fluences and solar exposure have been modeled for selected hardware from the Long...
One of the primary causes of material degradation in low Earth orbit (LEO) is exposure to atomic oxy...
In the flight materials exposure data base extensive quantitative data is available from limited exp...
The LDEF mission was to study the effects of the space environment on various materials over an exte...
The Evaluation of Oxygen Interactions with Materials 3 (EOIM-3) flight experiment was developed to o...
The definition of LDEF atomic oxygen exposure involves theoretical prediction of fluxes, modeling of...
Power degradation in the solar cells was consistent with the exposure environment and appears to be ...
The atomic oxygen flux exposure experiments flown on Space Shuttle flights STS-5 and STS-8 are descr...
Thermal control coatings within the recessed compartments of LDEF Experiment A0034 experienced the m...
Contamination that leads to degradation of critical surfaces becomes a vital design issue for many s...