AEROSPACE SYSTEM Russian patent published in 2010 - IPC B64G1/00 B64D5/00 F41F3/42 

FIELD: transport.

SUBSTANCE: invention refers to rocket and space equipment. Aerospace system includes carrier aircraft, carrier rocket and pay load, which are carried with the aircraft and arranged in heat-insulated transporter-launcher container and fixed in it by means of mounting elements, as well as carrier rocket booster staging system. Transporter-launcher container of carrier rocket is made in the form of two longitudinal semi-doors which are symmetrical relative to vertical plane and connected in the upper joint of longitudinal joints with hinged connection, and is provided with mechanism for opening semi-doors and for extending the rocket beyond the semi-doors of transporter-launcher container to carrier rocket start position. Inside the transporter-launcher container the semi-doors are equipped with transverse mutually joining heat-insulated partitions adjacent to carrier rocket surface and dividing inner space of transporter-launcher container into compartments for the head end and for each of the carrier rocket tanks separately. Transporter-launcher container is equipped with support system of stable thermal mode of carrier rocket content by means of control valves used on walls of compartments of transporter-launcher container for additional provision of temperature mode in compartments by controlling the intensity of bypass of thermostabilising gas to the gap between walls of tanks of carrier rocket and walls of the appropriate compartments of transporter-launcher container.

EFFECT: reducing thermal action and action of impact loads on carrier rocket.