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Used
for simulating the outer-space thermo-vacuum environment.
Space-aircraft or other equipment for experiment can
be put in the vacuum chamber. The system can be used
for the thermo-vacuum experiment, thermo-cycle experiment,
thermo-control experiment, anti-static experiment
and thermo-optical experiment, etc.
Inner size: ¦Õ1000mm, ¦Õ2000mm, ¦Õ3000mm
Ultimate pressure: coldness ( -173¡æ ¡« -60¡æ £© 1¡Á10
-5Pa; hotness £¨£« 100¡æ £© 1¡Á10 -4Pa
Temperature uniformity: ¡À5¡æ
Over 360 hours non-stop operation
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