Add to ORKGIn-situ monitoring of the Wide-Field/Planetary Camera, a Hubble Space Telescope science instrument, was performed in a vacuum environment to better understand the formation of ice on cooled optical detectors. Several diagnostic instruments were mounted on an access plate to view the interior of the instrument housing and the graphite epoxy optical bench. The instrumentation chosen and the rationale for choosing the instrumentation are discussed. In addition, the performance of the instrumentation during monitoring operations is discussed
The mechanical and optical properties of the metallized Teflon Fluorinated Ethylene Propylene (FEP) ...
Due to their low mass pocketqubes are relatively inexpensive to launch. This makes them ideal for th...
A 40 cm diameter mirror assembly was interferometrically tested at room temperature down to 250 degr...
Spacecraft optical components must be tested in vacuum chambers in order to achieve “space-like” con...
In 2017, the combined Optical Telescope Element and Integrated Science Instrument Module (OTIS) of t...
There is a need for continuous monitoring for molecular contamination in clean rooms where spaceflig...
Contamination control requirements for the Wide Field/Planetary Camera II (WF/PC II) are necessarily...
Epoxy/glass test specimens representing Scout fourth and fifth stage motor casings were prepared and...
Plasma cleaning experiments were completed on hydrocarbon contaminant films, experiments were initia...
Material outgassing in a vacuum leads to molecular contamination, a well-known problem in spacefligh...
NASA's In Situ Contamination Effects Facility, Marshall Space Flight Center, has been used to test s...
In 2017, the James Webb Space Telescope (JWST) underwent functional testing and optical metrology ve...
The state of contaminant molecules, the deposition rate on key surfaces, and the heat transfer rate ...
The contamination characters of selected materials used in space technology testing. Specific materi...
This presentation describes the thermal design of the three main of optical components which compris...
The mechanical and optical properties of the metallized Teflon Fluorinated Ethylene Propylene (FEP) ...
Due to their low mass pocketqubes are relatively inexpensive to launch. This makes them ideal for th...
A 40 cm diameter mirror assembly was interferometrically tested at room temperature down to 250 degr...
Spacecraft optical components must be tested in vacuum chambers in order to achieve “space-like” con...
In 2017, the combined Optical Telescope Element and Integrated Science Instrument Module (OTIS) of t...
There is a need for continuous monitoring for molecular contamination in clean rooms where spaceflig...
Contamination control requirements for the Wide Field/Planetary Camera II (WF/PC II) are necessarily...
Epoxy/glass test specimens representing Scout fourth and fifth stage motor casings were prepared and...
Plasma cleaning experiments were completed on hydrocarbon contaminant films, experiments were initia...
Material outgassing in a vacuum leads to molecular contamination, a well-known problem in spacefligh...
NASA's In Situ Contamination Effects Facility, Marshall Space Flight Center, has been used to test s...
In 2017, the James Webb Space Telescope (JWST) underwent functional testing and optical metrology ve...
The state of contaminant molecules, the deposition rate on key surfaces, and the heat transfer rate ...
The contamination characters of selected materials used in space technology testing. Specific materi...
This presentation describes the thermal design of the three main of optical components which compris...
The mechanical and optical properties of the metallized Teflon Fluorinated Ethylene Propylene (FEP) ...
Due to their low mass pocketqubes are relatively inexpensive to launch. This makes them ideal for th...
A 40 cm diameter mirror assembly was interferometrically tested at room temperature down to 250 degr...