COMPLEX–CONNECTED MODEL OF VACUUM GROUND LAUNCHING DEVICE OF THE LIGHT UNMANNED AERIAL VEHICLE

V.O. Sereda

For the purpose of revealing of features of working process, and also definition of a place and a role among other types of ground launching device (GLD) easy unmanned aerial vehicle (UAV) the in a complex–interfaced model of a vacuum catapult is offered. The model considers prevailing influence of wave factors on integrated characteristics GLD. The basic are presented thermogas–dynamic (physical fields of parameters in 3D–settlement area) and dynamic (distribution of speed and an overload on length directing) results of numerical modelling of the device. Unique properties of a vacuum drive and its possibility in comparison with other types GLD are noted.

Key words: launching device, unmanned aerial vehicle, compression expansion the car, vacuum drive, flexible transmission.