To investigate the aging behavior of fluoroelastomer FM-1D in hot air,with compression set as a parameter for seal aging,aging tests were conducted on fluoroelastomer FM-1D under different initial compression rates in a hot air environment ranging from 60℃to 150℃.The aging kinetic equation relating compression set of FM-1D to temperature and time was established,in order to predict its aging life at 25℃.The test results indicated that when the initial compression rate was 30%,the compression set exhibited an Arrhenius relationship with both test temperature and time.However,at a initial compression rate of 50%,the compression set gradually conformed to the Arrhenius relationship as time extended.These findings provide a reference for determining accelerated testing methods and maintenance cycles for FM-1D rubber materials.

Air lock module pressure control is a necessary step to balance the pressure inside and outside the spacecraft cabin and achieve the transfer of materials or personnel inside and outside the spacecraft cabin.The two main functions of the air lock module pressure control system are to reduce the pressure when leaving the chamber and increase the pressure when returning to the chamber.There are some methods such as releasing the gas in the chamber to vacuum or storing the gas in the chamber using containers.The control equipment for releasing gas is simple,but the gas is wasted.Gas storage requires temperature control and gas compressing equipment,but the gas is saved.There are some methods such as releasing gas from high-pressure vessels or releasing gas from nearby chamber.This article theoretically analyzes airlock module pressure controlling and provides several technical solutions for designing module pressure control systems.Releasing the gas to vacuum is suitable for spacecraft with a single sealed cabin while storing the gas is suitable for spacecraft with multi sealed cabins.Combined methods are also used in specific conditions.

Gathering together is an effectual way for improving quality and efficiency of the physical and chemical regenerative environmental control and life support system,as a regenerative gathering together technology,solid amine can simultaneously gather carbon dioxide and humidity with mild adsorption and desorption conditions,thus having the potential for miniaturization and low energy consumption,making it very suitable for manned deep space exploration missions.The current domestic and foreign systems cannot achieve perfect heat exchange between adsorption and desorption,resulting in low efficiency and less obvious comprehensive advantages.This study utilized multi-physics simulation methods to optimize system heat transfer,designed a combined control system for carbon dioxide and humidity,and verified various system characteristics such as flow rate and cycle time.The results show that:The designed porous thermal conductive medium can effectively reduce thermal resistance,and the obtained optimal filling ratio and structural size improve the heat transfer efficiency of the system.By adjusting the system characteristics,it is possible to dynamically satisfy the carbon dioxide and humidity control needs for 1～3 crews at different metabolic levels.This study verified the advantages of the regenerative combined carbon dioxide and humidity gathering system in terms of weight,power consumption,and volume,and obtained system characteristics,providing important technical support for manned deep space exploration missions.

To evaluate the aging life of silicone rubber sealing materials in the electrolytic water environment,the compression permanent distortion was taken as the performance change parameter of the sealing ring.Three typical silicone rubber materials,G146,G199,and 6144,were subjected to aging tests in the electrolytic water.The aging data was analyzed by the Arrhenius equation.And the aging kinetics equation of permanent compression deformation retention rate and temperature time was established,the aging life of silicone rubber sealing materials at 25℃was predicted.The results indicate the aging life of G146,G199,and 6144,was 21.3 a,9.8 a,and 12.0 a respectively.These prediction results provide a reference for determining the maintenance cycle of the sealing material.