NORINCO ZBKJ-1

History of the NORINCO ZBKJ-1

The ZBKJ-1 is a military aircraft designed for operations at medium to low altitudes, equipped with advanced optics and sensors for detailed battlefield imaging. It was introduced at the 2013 Xi'an International General Aviation Exhibition by Xi'an Zhongbing Space Technology Co., Ltd.

Featuring a double-arm design with a rear-mounted engine powering a two-bladed propeller unit, it has a main plane positioned above the fuselage in a straight line, along with fixed wheeled tricycle landing gear for stability.

The aircraft's lightweight yet durable composite structure houses movable optics at the front, enhancing its imaging capabilities. Performance specifications include a cruising speed of 100 mph, a service ceiling of 20,000 feet, and an 8-hour mission duration before recall, with an internal payload capacity of 175 lbs.

Launch options include catapult systems or self-powered takeoff, with the option for parachute-assisted descent or recovery on the same runway/airfield.

Ground control operations cover up to 136 miles, extendable to 250 miles via a communications relay system.

Specification

Basic

Year of Service: 2013

Origins: China

Status: Active.

Crew: 0

Production: 100+

Manufacturer: China North Industries Group Corporation (NORINCO) / Xi'an Zhongbing Aerospace Technology Co., Ltd. China

Carrier: China

Roles

Close Air Support (CAS): Designed to operate near active ground elements with a wide range of air-to-surface weapon and ammunition options.

Search and Rescue (SAR): Ability to locate and evacuate personnel from potentially hazardous or dangerous areas, such as downed pilots at sea.

Intelligence Surveillance Reconnaissance (ISR): Monitor ground targets/target areas to assess surrounding threat levels, enemy strength, or enemy movement.

Special Forces: Serve special forces/special operations forces and missions.

Unmanned: Aircraft designed (or later developed) have inherent unmanned capabilities and can fill a variety of battlefield roles.

Notable Features

Strong Aircraft Frame: The inherent ability of the airframe to take significant damage.

Extended range performance: Ability to travel long distances using on-board fuel supplies.

Unmanned operation: The design features the ability to fly without a pilot, with actions controlled by onboard programming and/or ground operators.

Camera equipment: Payload supports photographic devices that provide still and/or live image/video results.

Main Aircraft Structure

Monoplane: Designed to use a single main wing main aircraft; this is the most popular arrangement of main aircraft.

Shoulder: The main aircraft is mounted on the upper part of the fuselage, usually on an imaginary line that intersects the pilot's shoulders.

Straight: Floor plans involve the use of simple, straight main plan elements.

Performance

Installed: 1 x conventional engine unit located aft of the fuselage, in a thrust arrangement, driving the twin-blade propeller unit.

Maximum speed: 115 km/h (185 km/h | 100 knots)

Cruising speed: 99 km/h (160 km/h | 86 knots)

Maximum: 19,685 feet (6,000 m | 4 km)

Area: 621 km (1,000 km | 1,852 nautical miles)