MINI-REIS A FAMILY OF MULTIFUNCTIONAL UNMANNED LIGHT JET AIRCRAFTS
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1 National Aerospace University Kharkiv Aviation Institute KhAI Public Joint Stock Company "Kyiv Radio Plant" Inter-Industry Scientific & Research Institute of the Problems of Aircraft Flight Mode Physical Modelling MINI-REIS A FAMILY OF MULTIFUNCTIONAL UNMANNED LIGHT JET AIRCRAFTS Short Engineering Proposal Kharkiv
2 Mini-Reis: Timeliness of the Project At present, Ukraine does not have: aircraft false targets (imitators) to enhance the efficiency of aviation in case of active air defense of potential adversaries air targets to train air defense personnel effective means for air reconnaissance in an operation and tactical area effective means for destroying tactical and strategic unmanned aerial vehicles (UAV) and remotely-piloted aerial vehicles (RPAV) of potential adversaries
3 Mini-Reis UAV family: project objectives The project provides solutions to the existing challenges in Ukraine by developing a family of multifunctional unified light jet UAV (and a set of equipment based on its technology) that would provide for: defending the activities of front-line aviation with a help of light jet UAV as false targets (imitators) and generators of radio and infrared interferences training personnel of air defense facilities to use UAVs as aerial target performing reconnaissance (visual and radio-technical) in a tactical and operation area performing highly accurate attacks and destroying small-sized targets using warheads on board of UAV (miniature cruise missile) performing highly accurate attacks and destroying reconnaissance tactical and strategic UAVs of potential adversaries (UAV fighter based on the proposal developed by SRI PFM KhAI, Kharkiv and Donetsk, under the title Grif-Vulture ).
4 Mini-Reis: UAV family Mini-Reis S: takeoff weight up to 50 kg primary and secondary payload up to 10 kg flight duration of 30+ min motor thrust kgs analogues: ADM-160A MALD (USA), EWAL UAV 2000 (Israel) Mini-Reis M: takeoff weight up to 90 kg primary and secondary payload up to 20 kg flight duration of 30+ min motor thrust kgs analogues: ADM-160C MALD-J (USA) Mini-Reis L: takeoff weight up to 240 kg primary and secondary payload up to 60 kg flight duration of 30+ min motor thrust kgs analogues: ADM-141C ITALD (USA, Israel), Dan-ALC (Russia), Yabhon-GRN 1 (UAE), CL-289 (Canada, Europe)
5 Mini-Reis multifunctional family UAV usage: single use with potential self-destruction multiple use returning and parachute landing on inflatable shock absorbers UAV base variants: air external loads (up to 6) on a mother aircraft and air-based control station in a secondary cockpit land stationary and mobile on vehicle chassis with a land-based control station sea with a ship-based control station UAV launch variants: air-launched from external load sling of a mother aircraft jet-propelled from a launch container (incl. mass launch for a group usage up to 32 at a time) from a stationary or mobile pneumatic catapult
6 Mini-Reis modular primary and secondary payload Mini-Reis nose section can accommodate: Luneberg lens, generating radar cross section levels imitating aircrafts digital panoramic air cameras for optical reconnaissance in visible and infrared bands infrared and radiolocation target search and homing other equipment Mini-Reis center section can accommodate: chaff and flare dispenser radio electronic equipment of staging imitation and noise interferences for air defense systems radio reconnaissance station for recording emissions of SAM radio location stations and sending commands on targets radio equipment supplementary fuel tank parachute landing system warhead other equipment Mini-Reis tail section can accommodate: heat imitators (IR-tracers) smoke generators (smoke tracers)
7 Mini-Reis family unified components single aerodynamic scheme with similar key parameters (lifting surface loading, thrust-to-weight ratio) that cuts down expenses and time on aerodynamic tests unified components of onboard equipment single air-based control stations single land-based control stations single ship-based control stations
8 Specific aerodynamic concept of UAV family integral aerodynamic layout of an aircraft with a bearing body, that has strakes in front of a wing to achieve "vortex aerodynamic effects ease of folding the wings to place UAV in a launch container and as external load on a mother aircraft flat forms of UAVs (surfaces of small curvature) conformal high-mounted air intake of a power unit of the recessed type, gas dynamically integrated into the aircraft carrier system relatively small specific load on lifting surface area relatively high weight-to-thrust ratio a nozzle of the motors ejecting incoming air for shielding noises and IR radiation This specific aerodynamic concept provides for: high aerodynamic properties with a smaller lifting surface high maneuverability low visual, thermal and radar visibility while complying with the requirements for basic flight performance
9 Characteristics of some motors for Mini-Reis family Mini-Reis S Mini-Reis M Mini-Reis L Motor brand Olympus HP E (AMT, Netherlands) P200-RX (JetCat, Germany) TJ 40 (PBS, Czech Republic) P400-RX-G (JetCat, Germany) TJ 100 (PBS, Czech Republic) MC-100 (Motor-Sich, Ukraine) Max thrust, kgs Specific fuel consumption, kg/kgs*h Weight (with a startergenerator and other systems), kg Length,mm Diameter, mm Price, $ ? ~ ?
10 Mini-Reis UVA key dimensional, flight and other properties Mini-Reis S Mini-Reis M Mini-Reis L Weight, kg AV length, mm Wing span, mm Lifting surface area, m Max thrust, kgs Lifting surface loading, kg/m Launching thrust-to-weight ratio, kgs/kg Cruising velocity range, km/h (M) ( М) Max overload, g Max flight height, m Max flying distance, km 450 Max range, km 200 Development costs, $ ?? UAV costs, $ (mass produced in a basic configuration of its key systems; in a batch of 1,000 units) ?
11 Mini-Reis family weight report Mini-Reis S Mini-Reis M Mini-Reis L UVA dead weight (airframe), kg Power unit, kg Equipment and control (avionic), kg Propellant, kg Primary and secondary payload, kg, incl in a nose, kg in a center part, kg Construction margin, kg UVA takeoff weight, kg
12 Typical lay-out of Mini-Reis UVA Mini-Reis L layout
13 Scientific and engineering work plan to develop Mini-Reis UAV family STAGE WORK SCOPE DURATION DELIVERABLES COSTS, $ 1 Development of a technical task for scientific and engineering work and implementation of a conceptual project 2 Development of a preliminary design incl. tests of Mini-Reis UVA in T- 4 and T-6 wind tunnels at KhAI University 3 Engineering Design, inlc. development, production, bench and flight tests of a Mini-Reis S full-scale demonstrator 4 Development of a set of working design documentation for production and testing Mini-Reis S samples 1 year Technical Task and Conceptual Design documentation 1 year A set of documentation for Preliminary Design Stage 2 years A set of documentation for Engineering Design Stage, incl. analysis of the results of demonstrator flight tests 1 year A set of working design documentation - S Production and testing of Mini-Reis S samples 2 years Test reports and recommendations on amendments to working design documentation 6 Changes to working design documentation as a result of Mini-Reis S tests and marking the documents as S 1 6 months A set of working design documentation S Decision on commencing a mass production of Mini-Reis S and implementation of scientific and engineering work on Mini-Reis M and Mini-Reis L UAV? Decision? 8 TOTAL ~
14 Sincerely, Head of project development and implementation: Yatsenko Stanislav Yakovlevich, Director, SRI PFM KhAI Contacts: phone
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