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Microsatellite active heat controlling system based on LHP passive heat elimination

A technology of micro-satellites and thermal control systems, which is applied to devices for controlling the living conditions of aerospace vehicles, etc., can solve problems such as long-term oscillations in dynamic processes, life and reliability limitations, frequent shutters, etc., and achieve good steady-state performance, The effect of prolonging the service life and eliminating frequent vibration

Inactive Publication Date: 2009-09-02
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The early active thermal control system used temperature as the control reference quantity, and had good control characteristics in the steady state. However, when the external heat flow disturbance existed, the dynamic process would fluctuate for a long time, resulting in frequent movement of the shutters and excessive wear of the mechanical structure of the device. As a result, its life and reliability are limited, which is not conducive to its long-term use

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  • Microsatellite active heat controlling system based on LHP passive heat elimination
  • Microsatellite active heat controlling system based on LHP passive heat elimination
  • Microsatellite active heat controlling system based on LHP passive heat elimination

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Embodiment Construction

[0023] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0024] see figure 1 As shown, the surface of the micro-satellite facing away from the sun is generally provided with a heat dissipation surface radiator 2, the outer surface 21 of the heat dissipation surface radiator 2 is equipped with a thermal control louver 1, and the inner surface 22 of the heat dissipation surface radiator 2 is connected with the LHP condenser 4 mounted together. The outer surface 21 of the heat dissipation surface radiator 2 is coated with a thermal control coating with high emissivity and low absorptivity (the material of the thermal control coating can be F46 film aluminized or polyimide film aluminized), When the microsatellite is in orbit, the radiator 2 and the thermal control louver 1 are always facing away from the sunlight, and are used to dissipate the waste heat generated by the equipment and components in the microsatellite...

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Abstract

The invention discloses a microsatellite driving heat controlling system based on LHP passive heat elimination, which comprises a heat current temperature data processing module and an active heat controlling device, wherein the active heat controlling device has the structure that an LHP return flow channel and an LHP steam channel are respectively arranged between an LHP condenser and an LHP evaporator, a heat flow sensor is bonded between a heating device and the LHP evaporator, a temperature sensor A is arranged on the heating device, the LHP condenser is arranged on the inner surface of a radiating surface radiator, the outer surface of the radiating surface radiator is provided with grooves A and B, and temperature sensors are respectively arranged in the grooves A and B; the heat current temperature data processing module comprises a temperature channel deviation generating unit, a heat current channel deviation generating unit, a two-channel deviation signal fusing unit and a heat current and temperature control converting unit. The driving heat controlling system realizes the two-channel data fusion of the temperature and the heat current,, increases the response speed of the heat controlling system of the microsatellite, eliminates the frequent vibration of a heat control shutter, and prolongs the service life of the mechanical structure of the heat control shutter under the premise that the good steady-state performance of the heat controlling system is ensured.

Description

technical field [0001] The present invention relates to a thermal control system, more particularly to an active thermal control system for micro-satellites based on LHP passive heat dissipation. Background technique [0002] Microsatellites refer to microsatellites with a mass below 100Kg. Due to the design concept and manufacturing process of large-scale integrated circuits, microsatellites have the advantages of small size, light weight, and low manufacturing and launch costs. They are widely used in communications, military, and geological exploration. , Environmental and disaster monitoring, transportation, meteorological services, scientific experiments, deep space exploration and other aspects have a wide range of applications. [0003] In the microsatellite platform, the thermal control system plays an important role. When flying in orbit, the microsatellite works in a harsh external thermal environment. If no thermal control measures are added, a large change in the...

Claims

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Application Information

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IPC IPC(8): B64G1/50
Inventor 李运泽刘东晓王玉莹刘佳李运华王浚
Owner BEIHANG UNIV
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