METHOD OF THERMOSTATTING ROCKET POD OBJECTS AND ONBOARD SYSTEM FOR REALIZATION OF THIS METHOD Russian patent published in 2006 - IPC B64G1/50 F24F5/00 F24F13/06 

FIELD: methods and devices for thermostatting instrument module.

SUBSTANCE: injection of thermostatting medium into rocket pod is performed on side of its lateral surface symmetrically and at angle relative to vertical plane passing through plane of symmetry of location of rocket pod objects tangentially relative to the envelope of side surfaces of objects. Proposed system has holes for injection and escape of thermostatting medium with one-way valves and unit for injection of thermostatting medium. Thermostatting injection and escape holes are made in rocket pod shell. One-way valves of said holes are articulated in rocket pod shell. Unit for injection of thermostatting medium into rocket pod is made in form of subsonic diffuser provided with at least two bent branch pipes. Inlet section of diffuser is communicated with injection hole. Outlet sections of diffuser branch pipes are located in clearances between objects and rocket pod shell symmetrically relative to plane of symmetry of rocket pod passing through thermostatting medium injection hole. Tangent to axis of each branch pipe of diffuser in its outlet section is directed tangentially relative to the envelope of side surfaces of objects.

EFFECT: enhanced heat exchange on surfaces of objects during pre-launch preparation of rocket pod; reduced mass of onboard thermostatting system.

3 cl, 5 dwg