FIELD: rocketry. SUBSTANCE: chamber includes housing with nozzle, injector head, adapter engageable with nozzle insert made heat-resistant material integral with wall of combustion chamber. Nozzle insert is mounted at space relation to housing of chamber and is secured to injector head through additional adapter consisting of two rings made different materials and connected through spacer. EFFECT: enhanced efficiency. 7 cl, 8 dwg
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