FIELD: rocketry and space engineering; arrangement and mounting of equipment. SUBSTANCE: instrumentation section includes ferrule of rocket body with rectangular frames on which flexible hermetic bag is secured; bag is provided with locking member and drain holes. Cavity of one of frames is pressurized. Its wall is provided with hole for connection with on-board or surface thermostating system by means of pipe line; opposite wall has hole closed by air sprayer. Frames are provided with projections for mounting instruments with vibration isolators and struts for laying the cables and securing the bags. EFFECT: enhanced reliability. 4 dwg
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