@
S.U.R.B.
Probably trainers, COINs, and UAVs, as well as weapons for aircrafts.
Lasta 95 trainer
The Aircraft «LASTA» is designed for flight familiarization, evaluation of flying ability, pilot primary and basic training, primary instructions, acrobatics, formation flying, navigation, instrument and night flying. It can perform basic training in gunnery, rocket firing and bombing, also.
SPECIFICATIONS
Power plant:
- one engine ''AVCO-LYCOMING AEIO-540- L1.B5D" 224 kW (300hp), or optionally AVCO-LYCOMING AEIO-580-B1A 235 kW (315 hp)
- propeller two blade, variable pitch, constant speed HARTZELL HC-C2YR-4CF/FC 8475-6, or HARTZELL HC-C2YR-4CF/FC 8475-8
Dimensions:
- Wing Span: 9.702 m
- Length Overall: 7.965 m
- Height: 2.84 m
- Wing Area: 12.9 m2
Weights:
- Empty Equipped: 888 kg
- Max. Fuel: 130 kg
- Max. Take Off (Utility category): 1210 kg
- Max. Take Off (Aerobatic category): 1145 kg
Operational Capabilities (at max. TOF)
Speed:
- Maximum at S/L: 320 km/h
- Never Exceed: 390 km/h
- Maximum Rate of Climb at S/L: 8.5 m/s
Other characteristics:
- Service ceiling: 6000 m
- T-O Run: 300 m
- Landing Run: 280 m
- Maximum Range (without fuel reserve): 1160 km
- Maximum Flight Duration (without fuel reserve): 3 h
- Limit Load Factor: +6/-3
Kobac COIN
The Kobac is prototype of light military trainer aircraft in development by UTVA. It is a single-engine, low-wing tandem-seat turboprop training aircraft with a metal airframe. The aircraft will be capable of higher basic training functions including aerobatics, instrument, tactical flying and it provides an easy transition to jet trainer at higher training levels. And also will be capable of performing close air support, counter insurgency (COIN), and reconnaissance missions. Kobac in Serbian is the Sparrowhawk.
Specifications (Kobac prototype)
General characteristics
Crew: Two, student and instructor
Empty weight: 1,325 kg (2,921 lb)
Gross weight: 1,700 kg (3,748 lb)
Powerplant: 1 × Pratt & Whitney Canada PT6A-62 turboprop, 857 kW (1,149 hp)flat-rated at 708 kW (950 shp)
Performance
Maximum speed: 555 km/h (345 mph; 300 kn)
Cruising speed: 500 km/h (311 mph; 270 kn) at 7,620 m (25,000 ft)
Stall speed: 143 km/h (89 mph; 77 kn) EAS flaps and gear up, 128 km/h (80 mph; 69 kn) flaps and gear down
Range: 1,537 km (955 mi; 830 nmi)
Service ceiling: 11,580 m (37,992 ft)
g limits: + 6.0 g to -3.0 g
Rate of climb: 20.8 m/s (4,090 ft/min)
Take-off distance over 50 ft (15 m) obstacle at sea level: 1,280 ft (296 m)
Landing distance over 50 ft (15 m) obstacle at sea level: 2,295 ft (510 m)
Tactical UAV Pegaz
Long range tactical UAV for day and night reconnaissance and surveillance missions, target acquisition and designation. Equipped with single payload (up to 40 kg on the central adjunction point) or two different (up to 30 kg on the rear and up to 10 kg on the front adjunction point) provides flexibility to fulfill any kind of mission.
Тechnical data
Engine: Two cylinders boxer, 32 КW (43 BHP)
Propeller: Wooden two blades, pusher
Wing span: 6.34 m
Wing area: 4.24 m
Length: 5.395 m
Empty weight: 120 kg
Max payload weight: 40 kg
Max takeoff weight: 230 kg
Max speed: 200 km/h
Cruising speed: 130-150 km/h
Service altitude: 3000 m
Flight duration: 12 h +
Takeoff: Automatic from prepared runway (optional: catapult)
Landing: Automatic on prepared runway (emergency: parachute)
Range: 100 km
Guiding: Fully autonomous way points tracking, holding, camera guiding Emergency and return home mode Altitude and velocity autopilot
Short Range Tactical UAV ‘‘Sparrow’’
Tactical UAV for day or night reconnaissance and surveillance short range missions (up to 10 km) carrying EO payload (daylight or IR camera on the gyro stabilized platform) up to 1.5 kg.
Technical characteristics and performances
Engine: DC electric, 800 W
Propeller: Two blades, graphite composite
Battery: Li-Po 28V, 8000mAh
Wing span: 2.806 m
Wing area: 0.75 m2
Length: 1.94 m
Weight (without payload): 5.5 kg
Maximum payload weight: <1.5 kg
Max takeoff weight: 7 kg
Max speed: 120 km/h
Cruising speed: 61 km/h
Operational altitude (AGL): 300 - 500m
Flight duration: 1+ h
Launching: Automatic, hand launch
Landing:
- Automatic, parachute and airbag
- Optional: belly landing
Uplink: UHF, frequency-hopping spread spectrum
Downlink: S-band, digital, coded
Guiding: Fully autonomous way points tracking, holding, camera guiding
- Emergency and return home mode
- Altitude and velocity
Weaponry for helicopters, we sold them to Iraq recently
MULTI-SENSOR INTELLIGENT PLATFORM – MIP 11
The main application of system MIP is passive intelligence, surveillance and acquisition of moving and stationary objects in daily, night and low visibility conditions, in a move or in a stay position.
System includes multiple sensors which observe an area of interest and establish its electronic image in different parts of the electromagnetic spectrum. These groups combine multisensors complementary sensor fusion in order to efficiently solve the partial data base problem - passive or semi-active acquisition of facilities. The resulting multispectral image scene is corresponding to the actual situation in the area and can be distributed in real time to other users via the network.
Sensor system is placed on automatized ruggedized telescopic masts in various sizes and remotely controlled stabilized and unstabilized carriers units with a possibility of precise moving in azimuth and elevation.
System integrates the following sensors:
- passive sensor for the visible part of the spectrum - (video camera),
- passive infrared sensor range (thermal imaging - camera),
- active and passive source of laser radiation sensor - for measuring the distance to the object (laser range finder),
- GPS for self-position determination,
- digital compass for orientation.
Also, in order to extend the range of visibility, it is planned further research program and analysis of the possible integration of other sensors such as:
- radar,
- sound goniometer system for accurate determination of sound- sources,
- radar detector, detector of infrared or laser radiation, and chemical and - biological detectors
The system MIP deals with following activities:
- an object detection (to obtain basic information about the existence of the object electronic image scene analysis)
- an object identification (to obtain information on the nature and type of building electronic image scene analysis)
- geo-location (determining the absolute or relative position of the object in relation to the OE system).
- putting object’s position (coordinates) in the geographic information system (GIS).
- further data distribution to C4ISR system at а higher level