FIELD: rocketry; construction of dry compartments for various instruments of launch vehicles. SUBSTANCE: launch vehicle compartment has envelope with cuts and longitudinal and transversal primary structure in form of stringers and end and intermediate frames. Envelope is provided with two brackets secured at opposite ends of cut and connecting member of adjustable length which is secured in said brackets. Connecting member is made in form of rod with threaded tips at both ends for securing the rod to brackets through spherical articulations. Cut is framed by intermediate frames and strengthened stringers. Brackets are secured to ends of stringers. Brackets are secured with frames. Tips are provided with lock nuts. EFFECT: facilitated procedure of manufacture; ease in maintenance. 6 cl, 4 dwg
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