LIU Ming, HOU Zuo-xun, GAO Yuan. Design and Implementation of High Reliability Space Lighting Equipment[J]. 2022, 27(3): 105-110.
DOI:
LIU Ming, HOU Zuo-xun, GAO Yuan. Design and Implementation of High Reliability Space Lighting Equipment[J]. 2022, 27(3): 105-110.DOI: 10.15938/j.jhust.2022.03.014.
Design and Implementation of High Reliability Space Lighting Equipment
LED is used as the light source of the lighting subsystem of the manned spaceflight vehicle for the first time. The application of LED lighting source meets the lighting requirements of astronauts' short-time extravehicular activities in the extravehicular space environment. The space lighting equipment outside the cabin needs to work in a more rigorous and complex space environment
which requires the lighting equipment to have high reliability. In order to solve these problems
the circuit of multiple groups of constant current tubes directly driving the series parallel hybrid LED bulb array is designed
and the aluminum substrate is used as the circuit board substrate to heat the circuit. Meanwhite
the light distribution lens is designed to conduct secondary light distribution for the LED array
making the lighting equipment meet the lighting index requirements. The lighting equipment has passed the environmental tests such as temperature cycling
aging
low-temperature start-up
life test and anti-irradiation total dose test. The lighting equipment is placed 2.5m away from the target for test. The test results show that the illumination field angle of the equipment is greater than 48°
the maximum illumination is 562.5lx
and the illumination uniformity is 56.3%
which meets the requirements of aerospace applications.