METHOD FOR TEMPERATURE CONTROL OF ONBOARD EQUIPMENT OF PAYLOAD LOCATED INSIDE HEAD FAIRING OF SPACE HEAD PART OF SPACE ROCKET, AND DEVICE FOR ITS IMPLEMENTATION Russian patent published in 2018 - IPC B64G1/00 

FIELD: astronautics.

SUBSTANCE: group of inventions relates to the aerospace equipment. Method of temperature control of the onboard equipment of the payload (PL) located inside head fairing (HF) of the space head part (SHP) of space rocket (SR), includes blowing a thermostatic medium into the inner space of HF, its flowing over along HF with subsequent expiration from it. Supply is carried out forcibly from the internal space of HF to the PL compartment through its injection hole with the subsequent outflow of the medium from the PL compartment to the internal space of the HF through the discharge hole. Injection of a thermostatic medium into the PL compartment is carried out only for a given range of medium temperatures in the inner space of HF. Method is implemented by a thermostatic device, which includes a hole for the injection of a thermostatic medium, a hole for its flow into the HF, and a device for the injection of a thermostatic medium into the internal space of the HF. In the maintenance hatch of the onboard equipment of the PL compartment, a removable cover is installed, in which an injection hole is made for the forced flow of a thermostatic medium by means of a fan.

EFFECT: technical result of the group of inventions is to increase the efficiency of temperature control.

3 cl, 2 dwg