Leak rate design method for sealed cabin of manned spacecraft
A technology of manned spacecraft and design method, which is applied in the field of leak rate design of manned spacecraft airtight cabin, and can solve problems such as the lack of top layer design of airtight cabin
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[0020] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0021] in, figure 1 is the specific flow chart of the design method for the cabin leakage rate of manned spacecraft, figure 2 It is a composition diagram of the sealing link of the airtight cabin of the manned spacecraft, image 3 It is a schematic diagram of the conversion relationship between mass leakage and leak rate.
[0022] like figure 1 As shown, the method specifically includes the following steps:
[0023] According to the system scheme design, the mission analysis is carried out on the flight mode of the manned spacecraft in the whole mission stage, and the mission time requirements of each flight stage are obtained;
[0024] Preliminary determination of the gas weight that the system can use for leakage compensation, and system weight analysis for manned spacecraft;
[0025] Preliminarily calculate the mass leakage of the se...
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