Product description
SNT-180 is a medium-speed target drone, which takes into account the training and equipment testing of the navy, army, and air force. It has the functions of one-key ignition, pre-planning routes, re-planning routes, and online uploading and switching routes at any time. It supports multi-aircraft formations, can simulate saturation attacks, can simulate the flight characteristics and radar characteristics of aircraft and cruise missile targets, and can be equipped with RCS A variety of loads such as enhanced equipment, infrared enhanced equipment, and active jamming equipment can be used for air defense training of antiaircraft artillery, missile units, and electronic jamming to meet the needs of army training and equipment testing of aerial targets.
System composition
The SNT-180 target drone system consists of the main parts of the body platform, flight control system (navigation, flight control, actuator, power supply system, etc.), telemetry and control system, fuel power system, booster rocket system, parachute recovery device and mission load. composition.
Features
With Beidou/inertial integrated navigation precise route control capability;
Support rocket-assisted zero-length takeoff, which can take off on the ground or at sea;
Support parachute landing + airbag recovery, with automatic parachute throwing function after recovery and landing;
It has complete safety protection functions such as autonomous security control, emergency response (automatically open parachute, hovering, self-destruction in emergency), one-key homing and self-destruction by command;
It has program-controlled flight capability, and can automatically and stably fly according to preset and online planned routes. The route supports online real-time revision and re-planning function, and the route can be manually edited and modified at any time during the flight.
It has commanded flight capability and can fly stably in accordance with ground control commands.
With parameter return function, real-time return flight parameters (attitude, altitude, airspeed, pointing, angular rate, latitude, longitude, speed, heading, etc.) and engine parameters (speed, temperature, pressure, etc.) to the flight controller and ground telemetry equipment.
The engine supports the ground station to remotely control one station electric start;
Communication frequency: different frequency bands can be used, and the working frequency points approved and filed by the Office of the Electromagnetic Spectrum Management Office of the whole army are preferred.
Support one-stop multi-aircraft fully automatic coordinated formation flying function, and support multiple tactical formations;
A variety of mission loads such as lumber ball, tracer tube, lotus seat, etc. can be installed;
Ultra-low-altitude sea-skimming flight capability, remote control and telemetry throughout the entire ultra-low-altitude flight;
Navigation/link anti-interference, safe flight under interference failure conditions;
The infrared-enhanced payload supports automatic ignition according to instructions or ignition according to instructions;
Equipped with night flight lights to support night flight.
Static parameter index
Length: 3.2m
Wingspan: 1.6m
Take-off weight: ≮90kg
Take-off method: land/sea shipboard assisted take-off
Recovery method: land parachute recovery/sea parachute recovery, floating at sea, full body waterproof
Basic flight performance
Maximum level flight speed: ≮190m/s
Maximum flying altitude: ≮10000m (altitude)
Minimum flight altitude:
Land: 20m (relative height)
At sea: 5m (ultra-low altitude sea skimming)
Endurance: ≮65min
Measurement and control radius: ≮150km
Formation capacity: 16 aircraft in one station, distance between aircraft ≥ 30m
Formation style: group formation, high-density formation, continuous multi-target, multi-directional simultaneous arrival
Target characteristics simulation
Load weight: ≮10kg
Load type: tracer tube, lumber ball, interference radiation source, seeker simulator, etc.
RCS: 0.1m2~3m2 (adjustable)
Motor overload: <4g
