Laser Radar Metrology Measurements through a Chamber Window of the James Webb Space Telescope Compon
July 13, 2010 at 10:00 am
Carson Rooms 2, 3 and 4, enter at Carson 2
Anthony Slotwinski - Representing Nikon Metrology Inc.
Abstract:
NASA’s James Webb Space Telescope (JWST), the successor to the Hubble Space Telescope, will be the premier space science program for astrophysics in the coming decade. Testing of both the subsystems of the telescope and the fully assembled unit is currently underway. Metrology measurements of critical subsystems under vacuum and cryogenic conditions are needed to ensure proper operation. However, current non-contact, laser based measurement systems cannot operate under these conditions. This paper presents the results of measuring through a vacuum chamber window using a Nikon Metrology (formerly Metris) Laser Radar.
The accuracy of laser metrology measurements depends upon knowing the parameters of the media through which the measurement beam travels. Under normal conditions, this means knowledge of the temperature, pressure and humidity of the air in the measurement volume. Typically, thermal gradients provide the most challenging aspect of achieving accurate measurements but this can be overcome with temperature sensors along the measurement path. Often, however, there is a need to measure an object in an environment unsuitable for the measurement instrument, such as in an extreme temperature environment. In the past, windows have been used to protect the measuring device from the heat of the molten metal in a steel mill but, due to the relaxed accuracy requirements, a rigorous model of the effect of the window on the measurement was not done.
In the case of the James Web Space Telescope components, high accuracy measurements through a window must be made with the components at cryogenic temperatures in a vacuum. The ability to make accurate measurements through a window presents a challenge as there are a number of factors to considerer. In the case of the laser radar the window will increase the time-of –flight of the laser beam causing a ranging error, and refract the direction of the beam causing angular positioning errors.
A model is being developed to compensate for these effects and for the fact that part of the measurement path is in vacuum. Parameters being considered include the window material, thickness and shape. In addition, differences in pressure, temperature, and humidity on each side of the window will cause slight atmospheric index changes and induce deformation and a refractive index gradient within the window. Also, since the window is a dispersive media, the effect of both phase and group indices have to be considered. Ambient measurements taken on a target-filled test piece showed good agreement with the model. Cryogenic/vacuum measurements include an array of targets matching the laser radar's capabilities: holes, tooling balls, and various scan areas. These measurements are taken at specific points throughout the cycle of the cryogenic experiment and matched to modeling. Those measurements points are: without the window in place, with window at ambient, with window at vacuum, and at cryogenic temperature. This paper discusses our findings.
Carson Rooms 2, 3 and 4, enter at Carson 2
Anthony Slotwinski - Representing Nikon Metrology Inc.
Abstract:
NASA’s James Webb Space Telescope (JWST), the successor to the Hubble Space Telescope, will be the premier space science program for astrophysics in the coming decade. Testing of both the subsystems of the telescope and the fully assembled unit is currently underway. Metrology measurements of critical subsystems under vacuum and cryogenic conditions are needed to ensure proper operation. However, current non-contact, laser based measurement systems cannot operate under these conditions. This paper presents the results of measuring through a vacuum chamber window using a Nikon Metrology (formerly Metris) Laser Radar.
The accuracy of laser metrology measurements depends upon knowing the parameters of the media through which the measurement beam travels. Under normal conditions, this means knowledge of the temperature, pressure and humidity of the air in the measurement volume. Typically, thermal gradients provide the most challenging aspect of achieving accurate measurements but this can be overcome with temperature sensors along the measurement path. Often, however, there is a need to measure an object in an environment unsuitable for the measurement instrument, such as in an extreme temperature environment. In the past, windows have been used to protect the measuring device from the heat of the molten metal in a steel mill but, due to the relaxed accuracy requirements, a rigorous model of the effect of the window on the measurement was not done.
In the case of the James Web Space Telescope components, high accuracy measurements through a window must be made with the components at cryogenic temperatures in a vacuum. The ability to make accurate measurements through a window presents a challenge as there are a number of factors to considerer. In the case of the laser radar the window will increase the time-of –flight of the laser beam causing a ranging error, and refract the direction of the beam causing angular positioning errors.
A model is being developed to compensate for these effects and for the fact that part of the measurement path is in vacuum. Parameters being considered include the window material, thickness and shape. In addition, differences in pressure, temperature, and humidity on each side of the window will cause slight atmospheric index changes and induce deformation and a refractive index gradient within the window. Also, since the window is a dispersive media, the effect of both phase and group indices have to be considered. Ambient measurements taken on a target-filled test piece showed good agreement with the model. Cryogenic/vacuum measurements include an array of targets matching the laser radar's capabilities: holes, tooling balls, and various scan areas. These measurements are taken at specific points throughout the cycle of the cryogenic experiment and matched to modeling. Those measurements points are: without the window in place, with window at ambient, with window at vacuum, and at cryogenic temperature. This paper discusses our findings.
