The paper is devoted to the experimental studies of the aerodynamic drag of staggered bundles of helical tubes in order to create highly effective heat exchangers with reduced weight and size. The researches of the aerodynamic drag of staggered bundles of helical tubes at their airflow were carried out on an experimental setup, which is an open-circuit wind tunnel of rectangular cross section and conducted by the method of physical modeling in an isothermal flow, using the data of the drainage selection of static pressures before and after the bundle. The influence of geometric characteristics of helical tubes and parameters of their placement in the bundle on the aerodynamic drag is shown. The comparison of the aerodynamic drag of the bundles of helical and plain tubes of the same outside diameter depending on the incident velocity was conducted. The research results can be used in developing recuperative heat exchangers having high heat-aerodynamic efficiency and applied in thermal power engineering, petrochemical industry, gas compressor units of the gas transportation system ofUkraine. The obtained results can be the basis for aerodynamic calculations in the design of new heat exchangers of helical tubes.