This invention discloses a method,
system, equipment, and medium for testing the airtightness of a stratospheric airship
capsule. The
system includes a
capsule inflation device, a
capsule volume measurement device, an environmental parameter measurement subsystem, a capsule parameter measurement subsystem, and a
data transmission and storage subsystem. The method establishes the relationship between the volume of the capsule under test and the internal and
external pressure difference. It measures the
internal temperature of the capsule, the internal and
external pressure difference, the ambient temperature, and the
ambient pressure under different initial
pressure difference conditions to obtain the equivalent pore
size value for gas leakage under different pressure differences. Based on the
flight test design conditions of the stratospheric airship, the gas leakage amount is calculated daily for each day and night during the
stationary phase, and the capsule volume, capsule
pressure difference, and equivalent pore
size value are updated for each day and night until the capsule
pressure difference is less than a preset minimum pressure difference value, thus reaching the theoretical stationary time, thereby obtaining the airtightness test results of the stratospheric airship capsule. This invention can improve the accuracy of evaluating the airtightness performance of stratospheric airship capsules.