The invention relates to a hydraulic ejection 
system for an unmanned aerial vehicle. The hydraulic ejection 
system comprises a hydraulic driving part, a hydraulic 
energy storage part, a hydraulic starting part, a hydraulic buffering part, a 
hydraulic brake part, a hydraulic 
oil tank and a hydraulic pipeline for being connected between the hydraulic drive part, the hydraulic 
energy storage part, the hydraulic starting part, the hydraulic buffering part, the hydraulic braking part and the hydraulic 
oil tank, wherein the hydraulic driving part comprises a motor, a 
variable capacity pump, hydraulic motors and an electro-hydraulic directional control valve 18; the 
energy storage part comprises energy accumulators, an electromagnetic 
relief valve and a pressure gage; the hydraulic starting part comprises a starting 
hydraulic cylinder and an electro-hydraulic directional control valve 6; the hydraulic 
cushioning part comprises a 
cushioning hydraulic cylinder and an electro-hydraulic directional control valve 7; the hydraulic braking part comprises a braking 
hydraulic cylinder and an electro-hydraulic directional control valve 5; the energy accumulators are connected with the hydraulic motors in series, and besides, a control valve group is connected to the hydraulic pipeline between the energy accumulators and the hydraulic motors in series; besides, a 
brake valve group and a prefill valve are arranged on the hydraulic motors; besides, the control valve group is connected with the 
brake valve group. The hydraulic ejection 
system disclosed by the invention is high in drive force, rapid in 
cushioning and braking, stable and reliable in properties, and adaptive to operating requirements for different take-off weights and different take-off speeds of different unmanned aerial vehicles.