Description

Airborne target robotic complex «STRELA» is designed for performance of a wide range of tasks:

- flying around anti-aircraft missile systems (AAMS) with the aim of training the crew in working conditions for various types of targets;

- assessment of actual, but not declared in technical specifications, performance characteristics of firing radars (AMIS: air missile interception system): target detection range with various reflecting surface efficiency (RSE), accuracy of tracking such targets in terms of distance, speed and angular coordinates;

- assessment of accuracy of geodetic connection and orientation of firing RS AAMS significantly influencing upon efficiency of target designation from external systems;

- firing tests AAMS(AMIS);

- assessment of actual reflection characteristics of airborne vehicles within the range of wavelength AAMS(AMIS);

- airborne target «STRELA» is a full analogue of actual targets in terms of almost whole list of parameters topical for firing RS and RF homing heads (length, speed, angular coordinates, RSE);

- use of «STRELA» ensures significant decrease of material expenses for settlement of tasks listed above, because performance of expensive flights using actual airborne vehicles is not required. Besides, complexity and labor intensiveness significantly decreases with regard to organization of flight experiments;

Characteristics

Engine turbojet

Statistical traction N 9-220

Engine speed rev/min 32000-112000

Fuel consumption ml/min 129-730

Speed of exhaust gas at nozzle section km/h 1840

Parachute rescue system (designed for emergency landing)

Max.(barometric) height for activation of the parachute system m 3500

Vertical speed of UAV descent above sea level with the following characteristics х in МСА circumstances m/s not more than 5

Maximum speed for activation of the parachute m/s 60

Minimum speed for activation of the parachute m/s 15

Minimum height of parachute activation above the landing field level m 100

Barometric height of location of the area above sea level m up to 2000

Key geometric characteristics

Length mm 2384

Span of wings mm 2800

Weight data

Takeoff mass kg 33

Standard fuel margin ml 7200

Basic flight characteristics

Range of horizontal flight speed km/h 100-330

Maximum speed with extended landing gear km/h 290

Cruise speed km/h 150

Required traction at cruise speed N 60

Takeoff speed km/h 90

Landing speed at glide path with extended flaps km/h 115

Vertical speed during landing m/s 5-6

Contact velocity km/h 85

Flight attitude range m 50-3000

Practical flight length km 90

Flight duration minutes 20

Control

Flight control Automatic/dual

Communication range (within line of sight) km up to 64

Control system Autonomous navigation, automatic performance of the flight task