FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to shortened aircraft take-off systems. Launching installation includes light-weight power frame (2) with reduced carrying capacity. Power frame (2) is designed for loads from mobile starting installation and load from transfer of horizontal pulse of motion to aircraft (3). Chassis (1) of mobile starting unit is made light-weight, and carrying capacity of chassis (1) is reduced. Docking attachment (4) of mobile start-up unit with aircraft (3) attached to power frame (2) is made for transfer of horizontal component of mechanical loads to aircraft (3). Accelerating jet propulsion unit (6) is installed on power frame (2). Fuel tank (5) installed on power frame (2) and connected by at least one fuel line with accelerating jet propulsion unit (6) is made smaller. Braking system including thrust reverser of propellant jet propulsion unit additionally comprises lightweight braking unit (9) of chassis (1), made with reduced power consumption. Mobile start-up unit includes control system.
EFFECT: higher mass and mass efficiency of take-off and braking.
3 cl, 2 dwg
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Authors
Dates
2020-12-24—Published
2020-01-20—Filed