FH-96 Long-Flight UAV System

Vue d'ensemble

Fh-96 UAV system consists of aircraft sub-system, measurement control and information transmission, transmission sub-system, task payload sub-system, command and information sub-system, launch and recovery sub-system and integrated support sub-system. The system adopts ejection take-off and skyhook recovery, which can realize zero-length launching. It can be used in narrow and rugged space, such as islands, reefs and warship; It can take off and recover in high-temperature environment; It can accompany combat forces, and also independently perform reconnaissance and surveillance tasks. Max. take-off weight: 35kg Max. flight speed: 120km/h Take-off/Recovery mode: Ejection/Skyhook or gliding Fully-autonomous, semi-autonomous and manual-control functions Redundant design of navigation equipment Flight control management has the ability of fault detection and isolation Command control and information processing system adopts portable design form

Spécifications techniques

Caractéristiques principales : Max. take-off weight 35kg, Max. flight speed 120km/h, Radius 100km, Endurance 15h/, Ceiling 4000m, Take-off/Recovery mode Ejection/Skyhook or gliding.

Spécifications techniques

Documentation