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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