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The RASL optical tube assembly also presented additional
design and fabrication requirements including high strength
to withstand the "G" loading of the aircraft
and operation in any attitude. The mirror supports have
to support the mirrors and maintain collimation (optical
alignment) over the various "G" loads, directions,
and temperatures. The wide temperature range requires
the mirror supports and the mirror optical spacing to
be fully passively temperature compensated.
DFM Engineering has used Invar (a metal with very low
temperature expansion coefficient) spacers on most of
their telescopes to minimize the focus shift with temperature
changes. The RASL telescope required Invar spacers and
additional temperature compensating elements to meet
the focus stability requirement. Additional information
on focus stability may be reviewed at "Performance
Requirements for the Internet Telescope".
NASA will soon be integrating the RASL telescope with
the Nd:YAG laser transmitter and the multi-channel filter-detector
receiver. Laboratory tests and demonstrations will be
followed by installing the RASL telescope into the airplane.
For more information on the original requirements and
design specifications from NASA, please visit our related
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Performance
Requirements for the Internet Telescope
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