In order to experimentally confirm theoretical hypotheses and confirm the feasibility and effectiveness membrane dryers in temperature control systems of launch complexes using, an appropriate experimental testing plan was developed. The experimental testing included three stages: preliminary laboratory research, field experimental testing, and clarifying educational and laboratory research. The purpose of the research is to perform a membrane drying technologies experimental development in the launch rocket complexes temperature control systems. The article discusses the composition, order, and stages of testing theoretically determined membrane drying principles necessary to confirm in relation to the launch rocket complexes temperature control systems. The temperature control systems with membrane drying existing designing methods, experimental, and educational laboratory stands schemes and designs are described. The scientific innovation of the research consists in the development of experimental development plan that allows to obtain a proven technology integrated into promising projects for the development of ground-based space infrastructure, as well as into educational programs for the timely training of qualified personnel and further design of modern temperature control systems by industry enterprises.