www.itwl.pl AIR FORCE INSTITUTE OF TECHNOLOGY 1st Category Institute in classification of MS&HE 01-494 WARSAW, PO Box 96 6 Księcia Bolesława Str. tel. + 48 22 685 20 01 fax. +48 22 685 22 99 e-mail: poczta@itwl.pl www.itwl.pl

MISSION INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY MISSION Scientific support of and research into problems of operating the military products of aeronautical engineering 2

INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY Our place in military scientific environment Ministry of National Defense Ministry of Science and Higher Education Air Forces military academies military universities Financing of the articles - defined activity aeronautical research problems Air Force Institute of Technology Department for Armament Policy tasks military research centers

INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY Division for C4ISR Systems Integration Division for Aeronautical Systems’ Reliability and Safety Division for Aircraft Division for Propulsions Division for Avionics AWIONIKA Division for Air Armament Division for Airfield Systems Division for C2 and Training Systems Division for Fuels and Lubricants 4

INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY ROLE and PLACE in aviation environment CONCEPT DESIGNING PROTOTYPE TESTS’ PARTY SERIAL PRODUCTION USAGE MAINTENANCE STORAGE REPAIR & OVERHAUL UPGRADE UTILIZATION EXPLOATATION RESEARCH AREAS Diagnostics and monitoring Avionics Computerized Management Systems Air Armament UAV’s In-flight and on-ground tests Simulation and modelling Airfields pavement and systems Training systems Fuels and working liquids

ACCREDITED RESEARCH LABORATORIES INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY ACCREDITED RESEARCH LABORATORIES Laboratory for Mechanical and Climatic Hazards Laboratory for Pressure Measuring Laboratory for Health Monitoring of Fluid-Flow Machines Laboratory for Working Liquids Laboratory for Materials Strength Testing Laboratory for Aeronautical Structures dedicated Materials Testing 6

Laboratory for Pressure Measuring INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY Laboratory for Pressure Measuring The Laboratory carries out calibration of pressure gauges and monitoring systems & measuring devices used for checking on-board pilotage and navigational systems; altimeters, speedometers, Machmeters and variometers.

Laboratory of Non Destructive Testing Magnetic particle inspection Penetrant inspection Shearography inspection Water inclusions in a honeycomb structure Eddy current inspection Acoustic inspection: mia, pitch-catch, resonance Visual inspection D-SIGHT inspection Ultrasound inspection

Flying Laboratory INSTYTUT TECHNICZNY WOJSK LOTNICZYCH Aircraft AIR FORCE INSTYTUTE OF TECHNOLOGY Flying Laboratory Aircraft - bi-seat, piston engine, day and night flights; - research systems on board: Max speed > 270 km/h; Cruising speed (0,75 MCP) 240 km/h; Radius > 600 km; Endurance > 2,5 hrs; Payload > 100 – 150 kgs interferometer spectrometer pollution & contamination measurement system research pod additional equipment external fuel tank Movable head with infrared and video cameras Independent measurement system flight parameters recording system + camera; video and flight parameters transmission system; digital video (infrared) camera system; stabilized turret control & video transmission systems; independent power supply system for researching elements; avionic systems using data bar MIL-STD-1553B & ARINC-429; 2 under wing pylons for external measurt systems (up to 50 kgs) + 1 pylon under the fuselage.

UAVs INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY UAVs

The UAV System INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY The UAV System Endurance 1.5 h Cruising speed 90 km/h Max speed 135 km/h Operational radius 20 km On-board equipment Variant: 1) stabilized turret with a digital camera, 2) stabilized turret with an infrared camera, including an image transmission system in real time.

The UAV System INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY The UAV System On-board equipment Variant: 1) stabilized turret with a digital camera, 2) stabilized turret with an infrared camera, including an image transmission system in real time. Endurance 45 mins Cruising speed 50 – 90 km/h Weight/load 5 / 1.2 kgs Operational radius 20 kms Op. Altitude 50-600 ms

THE AIRBORNE CAMERA-RECORDER POD INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY THE AIRBORNE CAMERA-RECORDER POD Certyfied in flght and ready to use for different purposes. Length 2300 mm Diameter 340 mm Weight 100 kg Recording time >5 hrs (at -15° C) Power supply autonomous

The Stationary Terrain Surveillance System INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY The Stationary Terrain Surveillance System APPLICATION The Stationary Terrain-Surveillance System can be used to observe and keep close watch on selected areas and/or objects. Cameras included in the system can perform in different ranges of electromagnetic spectra (visible light and infra-red radiation), at different times of day/night, and under various weather conditions. The System consists of: Mobile mast Electro-optical surveillance turret Imagery-transmission system Operator's station Logistic-support providing equipment Container to house the operator's station

INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY COORDINATION CENTRE NETWORK CENTRIC CAPABILITIES SYSTEMS INTEGRATION

MOBILE RECORDING & MEASUREMENT SYSTEM TO RECORD ON THE GROUND IN FLIGHT TEST RESULTS OF THE EQUIPMENT AND AVIONIC ELEMENTS video image from board of the aircraft digital data in different displays

TRANSMISSION SYSTEM Airborne video image Serwisowanie odbiorników; Zabudowa odbiorników na pokładach jednostek naziemnych i statków powietrznych (integracja z systemami pokładowymi); Badania okresowe odbiorników systemu GPS; Opracowanie, badania i analizy nowych technik wykorzystania systemu GPS; Opracowywanie, badanie i analizy nowych aplikacji systemów GPS, GLONASS, Galileo, QZSS;

A S I M S INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY A S I M S AIRCRAFT STRUCTURAL INTEGRITY MONITORING SYSTEM DATA TRANSMISSION SYSTEM AVIONICS AND COMMUNICATION SYSTEM INTEGRATION

ASIMS structural problem (failure, cracking, yielding ,etc.) INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY ASIMS structural problem (failure, cracking, yielding ,etc.) defining corrective actions flight program decisions tests of structural modifications or changes

ASIMS maintenance knowledge of the required actions INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY ASIMS maintenance knowledge of the required actions differences from original design usage technical support

Avionic Systems’ Integration INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY Avionic Systems’ Integration

Integration of communication systems INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY Integration of communication systems

GPS Receiver service; Receiver installation Periodic tests; INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY GPS Receiver service; Receiver installation Periodic tests; New techniques application; New applications for GPS, GLONASS, Galileo, QZSS

The survival/immersion suit INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY The survival/immersion suit

OUR TRUMPS Certificated personnel Certificated laboratories Experience in development and implementation of aircraft structure and life cycle assessment programs Programs for technical support Stability in scientists and personnel Cooperation with industry and other R&D centers Technical support realized by AFIT is subordinated to MoND & MSHE 15

Thank you for your attention INSTYTUT TECHNICZNY WOJSK LOTNICZYCH AIR FORCE INSTYTUTE OF TECHNOLOGY Thank you for your attention