The present invention discloses a calibration
chip for a closed encapsulation structure for in-
orbit analysis of volatile substances in
lunar soil, which relates to the field of
aerospace technology, and solves the problems of opening and closing of passages in different scenarios, as well as the problems that in the existing calibration methods,
sample contamination and leakage may occur under the
impact during the launch, flight, and landing stages, affecting the analysis results, and the opening and closing of passages in different scenarios. The present invention includes a base, a gland, and a
hot melt foil. The gland is installed on the base to form a calibration cavity; a plurality of air holes are provided on the gland, and the
hot melt foil covers the air holes. After the
hot melt foil is heated and melted, a gas passage is formed between the calibration cavity and the gland through the air holes. The present invention opens the air hole passage by means of
induction heating and hot melting, effectively simplifies the structure of the calibration device, and makes the calibration process more accurate and efficient.