Basic parametersScope of application: Fixed wing unmanned aerial vehicles weighing 30-100kgMaximum initial ejection velocity: 40-50 m/s (velocity is related to weight, with lower weight resulting in higher velocity)Unfolding length: 9-12m (varies depending on the aircraft)Launch system power: high-p
Basic parameters
Scope of application: Fixed wing unmanned aerial vehicles weighing 30-100kg
Maximum initial ejection velocity: 40-50 m/s (velocity is related to weight, with lower weight resulting in higher velocity)
Unfolding length: 9-12m (varies depending on the aircraft)
Launch system power: high-pressure gas, adjustable from 0 to 1.6MPa
Dimensions of each section in the assembled version: (length x width x height) 4.2m x 0.5m x 0.5m, excluding support brackets
Foldable version size after folding: (length x width x height) 4.5m x 1.5m x 0.8m, excluding trailer height
Weight: 90kg pressure tank, 260kg rack, operated by 4 or more people; Upgraded version with trailer capability
Launch systems with different levels of weight can be customized according to different aircraft layouts to meet aircraft with different propeller sizes