MINI-REIS A FAMILY OF MULTIFUNCTIONAL UNMANNED LIGHT JET AIRCRAFTS

Size: px
Start display at page:

Download "MINI-REIS A FAMILY OF MULTIFUNCTIONAL UNMANNED LIGHT JET AIRCRAFTS"

Transcription

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

DSSI UAV. Unmanned Aerial Vehicle. Research & Development Project

DSSI UAV. Unmanned Aerial Vehicle. Research & Development Project UAV Unmanned Aerial Vehicle HISTORY AND SKILLS of Small UAV with electrically powered propeller Description of the solution: Airframe,electronics, 2 battery sets 1 spare Airframe, battery charger Transport

More information

Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business. Real-time Mechanism and System Simulation To Support Flight Simulators

Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business. Real-time Mechanism and System Simulation To Support Flight Simulators Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business Real-time Mechanism and System Simulation To Support Flight Simulators Smarter decisions, better products. Contents Introduction

More information

Т38 STILET. Air Defense Missile System

Т38 STILET. Air Defense Missile System Т38 STILET Air Defense Missile System T38 STILET ADMS T38 STILET ADMS The T38 STILET Air Defense Missile System (ADMS) is designed to defend Army units, industrial and military installations from all types

More information

Electric Penguin s philosophy:

Electric Penguin s philosophy: UNMANNED PLATFORMS AND SUBSYSTEMS Datasheet v 1.1 Penguin BE Electric Unmanned Platform Up to 110 minutes of endurance 2 with 2.8 kg payload 23 liters of payload volume Quick replaceable battery cartridge

More information

TECHNICAL SUPPORT ASSETS COMPOSITION

TECHNICAL SUPPORT ASSETS COMPOSITION T38 STILET ADMS T38 STILET ADMS The T38 STILET Air Defense Missile System (ADMS) is designed to defend Army units, industrial and military installations from all types of aerial attack assets flying at

More information

INSTYTUT TECHNICZNY WOJSK LOTNICZYCH Air Force Institute of Technology

INSTYTUT TECHNICZNY WOJSK LOTNICZYCH Air Force Institute of Technology 1953-2014 INSTYTUT TECHNICZNY WOJSK LOTNICZYCH Air Force Institute of Technology 01 Aircraft Engines Division Airworthiness Division IT Logistics Support Systems Division Aeroplanes & Helicopters Division

More information

In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led

In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led A-Level Aerosystems In 2003, A-Level Aerosystems (ZALA AERO) was founded by current company President Alexander Zakharov, since then he has led the company to be a leader in the micro UAV market in Russian

More information

Chapter 8. Example Point Design - Suppression of Enemy Air Defenses

Chapter 8. Example Point Design - Suppression of Enemy Air Defenses Chapter 8 Example Point Design - Suppression of Enemy Air Defenses In order to quantify the sensitivity of UAVs to potential technological advances and to define promising UAVs as precisely as possible,

More information

Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences

Jay Gundlach AIAA EDUCATION SERIES. Manassas, Virginia. Joseph A. Schetz, Editor-in-Chief. Blacksburg, Virginia. Aurora Flight Sciences Jay Gundlach Aurora Flight Sciences Manassas, Virginia AIAA EDUCATION SERIES Joseph A. Schetz, Editor-in-Chief Virginia Polytechnic Institute and State University Blacksburg, Virginia Published by the

More information

FLYEYE Unmanned Aerial System

FLYEYE Unmanned Aerial System FLYEYE Unmanned Aerial System FLYEYE Unmanned Aerial System About Flytronic FLYTRONIC is a dynamic modern engineering company focussed on developing Unmanned Aerial Systems to provide observation and reconnaissance

More information

neuron An efficient European cooperation scheme

neuron An efficient European cooperation scheme DIRECTION GÉNÉRALE INTERNATIONALE January, 2012 neuron An efficient European cooperation scheme I - INTRODUCTION 2 II - AIM OF THE neuron PROGRAMME 3 III - PROGRAMME ORGANISATION 4 IV - AN EFFICIENT EUROPEAN

More information

ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE!

ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE! ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE! My team specializes in fabricating airframes that s appropriate for testing unmanned aerial vehicle components. Our airframes are made of hybrid composite

More information

Predator B: The Multi-Role UAV

Predator B: The Multi-Role UAV Predator B: The Multi-Role UAV June 2002 Report Documentation Page Form Approved OMB No. 0704-0188 Public reporting burden for the collection of information is estimated to average 1 hour per response,

More information

Development of a Subscale Flight Testing Platform for a Generic Future Fighter

Development of a Subscale Flight Testing Platform for a Generic Future Fighter Development of a Subscale Flight Testing Platform for a Generic Future Fighter Christopher Jouannet Linköping University - Sweden Subscale Demonstrators at Linköping University RAVEN Rafale Flight Test

More information

PENGUIN B UAV PLATFORM

PENGUIN B UAV PLATFORM UNMANNED PLATFORMS AND SUBSYSTEMS Datasheet v.0 PENGUIN B UAV PLATFORM Penguin B platform ready for payload and autopilot integration 0+ hour endurance Fuel injected engine option Up to 10 kg payload capacity

More information

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles Stuart Boland Derek Keen 1 Justin Nelson Brian Taylor Nick Wagner Dr. Thomas Bradley 47 th AIAA/ASME/SAE/ASEE JPC Outline

More information

LUNAR INDUSTRIAL RESEARCH BASE. Yuzhnoye SDO proprietary

LUNAR INDUSTRIAL RESEARCH BASE. Yuzhnoye SDO proprietary LUNAR INDUSTRIAL RESEARCH BASE DESCRIPTION Lunar Industrial Research Base is one of global, expensive, scientific and labor intensive projects which is to be implemented by the humanity to meet the needs

More information

Weaponizing Small Unmanned Aircraft Systems. Cody Tretschok Capture Manager, Advanced UAS Weapons Advanced Missiles and Unmanned Systems

Weaponizing Small Unmanned Aircraft Systems. Cody Tretschok Capture Manager, Advanced UAS Weapons Advanced Missiles and Unmanned Systems Weaponizing Small Unmanned Aircraft Systems Cody Tretschok Capture Manager, Advanced UAS Weapons Advanced Missiles and Unmanned Systems Copyright 2011 Raytheon Company. All rights reserved. Customer Success

More information

THE KARANTANIA UNMANNED AERIAL SYSTEM

THE KARANTANIA UNMANNED AERIAL SYSTEM THE KARANTANIA UNMANNED AERIAL SYSTEM ABSTRACT Tomaž Meze, Bogo Štempihar, Mihael Grom MIBO MODLI d.o.o. Čevica 6, SI 1370 Logatec, Slovenia tomi.meze@siol.net, info@mibojets.com Tone Magister University

More information

Bild : Bernhard Mühr German Aerospace Center Flight Operations

Bild : Bernhard Mühr  German Aerospace Center Flight Operations German Aerospace Center Flight Operations Bild : Bernhard Mühr www.wolkenatlas.de Introduction DLR is Germany s aerospace research center and space agency with about 4700 employees in 31 research institutes

More information

Design and construction a flying wing unmanned aerial vehicles

Design and construction a flying wing unmanned aerial vehicles Design and construction a flying wing unmanned aerial vehicles Vasile Prisacariu 1, Mircea Boscoianu 2 SUMMARY: Unmanned aerial vehicles (UAV) are starting to represent a larger importance in the aerospace

More information

Small UAV A French MoD perspective and planning

Small UAV A French MoD perspective and planning Small UAV A French MoD perspective and planning French ISTAR segmentation portable transportable infrastructure System volume Tactical Small UAV Contact Combat Helicopters (MTI) Fighter Aircrafts Land

More information

Ejemplos de aeronaves existentes similares a las propuestas en los RFP 2007

Ejemplos de aeronaves existentes similares a las propuestas en los RFP 2007 Ejemplos de aeronaves existentes similares a las propuestas en los RFP 2007 UAV Sergio Esteban sesteban@us.es 1 Advanced Technologies and Engineering Co (Pty) Ltd (ATE). Vulture Production: Production

More information

1.1 REMOTELY PILOTED AIRCRAFTS

1.1 REMOTELY PILOTED AIRCRAFTS CHAPTER 1 1.1 REMOTELY PILOTED AIRCRAFTS Remotely Piloted aircrafts or RC Aircrafts are small model radiocontrolled airplanes that fly using electric motor, gas powered IC engines or small model jet engines.

More information

Modeling, Structural & CFD Analysis and Optimization of UAV

Modeling, Structural & CFD Analysis and Optimization of UAV Modeling, Structural & CFD Analysis and Optimization of UAV Dr Lazaros Tsioraklidis Department of Unified Engineering InterFEA Engineering, Tantalou 7 Thessaloniki GREECE Next Generation tools for UAV

More information

수직이착륙형고속비행무인기로임무효율성및운용편의성증대 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 / 속도 / 체공성능우월로임무효율성제고 ( 회전익대비 ) EO/IR, LRF 탑재및임무장비교체가능한다목적용무인기

수직이착륙형고속비행무인기로임무효율성및운용편의성증대 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 / 속도 / 체공성능우월로임무효율성제고 ( 회전익대비 ) EO/IR, LRF 탑재및임무장비교체가능한다목적용무인기 헬기처럼뜨고비행기처럼나는수직이착륙형고속무인항공기 KUS-TR 수직이착륙틸트로터무인항공기 천이비행 순항비행 천이비행 수직이륙 수직착륙 틸트로터천이비행 개요 제원 / 성능 수직이착륙형고속비행무인기로임무효율성및운용편의성증대 전장 3.5 m 최대속도 250 km/h 특징 전폭 5.2 m 순항속도 200 km/h 자동수직이착륙으로높은운용성 ( 고정익대비 ) 고도 /

More information

BY HOEYCOMB AEROSPACE TECHNOLOGIES. HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV

BY HOEYCOMB AEROSPACE TECHNOLOGIES. HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV BY HOEYCOMB AEROSPACE TECHNOLOGIES HC-330 HYBRID-POWERED ALL- ELECTRICITY DRIVEN four-rotor UAV Content SYSTEM SPECIFICATI- ON TYPICAL USING PROCESS OVERVIEW SUBSYSTEM SPECIFICATI- ON 1 OVERVIEW System

More information

A SOLAR POWERED UAV. 1 Introduction. 2 Requirements specification

A SOLAR POWERED UAV. 1 Introduction. 2 Requirements specification A SOLAR POWERED UAV Students: R. al Amrani, R.T.J.P.A. Cloosen, R.A.J.M. van den Eijnde, D. Jong, A.W.S. Kaas, B.T.A. Klaver, M. Klein Heerenbrink, L. van Midden, P.P. Vet, C.J. Voesenek Project tutor:

More information

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system:

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system: Idealized tilt-thrust (U) All of the UAV options that we've been able to analyze suffer from some deficiency. A diesel, fixed-wing UAV could possibly satisfy the range and endurance objectives, but integration

More information

Predator Program Office

Predator Program Office Predator Program Office Developing, Fielding, and Sustaining America s Aerospace Force Predator Program Overview 14 June 02 Lt Col Stephen DeCou ASC/RABP DSN:785-4504 Stephen.DeCou@wpafb.af.mil Report

More information

UAV, Catapults, Hovercraft

UAV, Catapults, Hovercraft , Catapults, Hovercraft Kharkov, 2009 11.04.08 1 Scientifically industrial systems LTD Overall information Since 1997 year design office "VZLET successfully works in the field of pilotless aircraft. With

More information

PIAGGIO AERO P.1HH HammerHead UAS

PIAGGIO AERO P.1HH HammerHead UAS Medium Altitude Long Endurance ISR Unmanned Aerial System Dimensions Span 15.600 m [51.18 ft] Length 14.408 m [47.27 ft] Height 3.980 m [13.05 ft] Areas Wing 18.00 m2 [193.75 ft2] Horizontal Tail 3.834

More information

Aeronautical Systems Center

Aeronautical Systems Center Aeronautical Systems Center Global Hawk Program Overview Michael Johnston 303 AESG/LG DSN: 787-4047 Comm: 937-255-4047 michael.johnston@wpafb.af.mil RQ-4A Global Hawk System Global Hawk: High-altitude,

More information

Production of Scientific and Production Center Unmanned Aircraft Systems and Technologies

Production of Scientific and Production Center Unmanned Aircraft Systems and Technologies State Scientific Institution PHYSICAL-TECHNICAL INSTITUTE OF NATIONAL ACADEMY OF SCIENCES OF BELARUS Production of Scientific and Production Center Unmanned Aircraft Systems and Technologies Physical-Technical

More information

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics 10.3 Presentation of results 10.3.1 Presentation of results of a student project 10.3.2 A typical brochure 10.3 Presentation of results At the end

More information

International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July ISSN BY B.MADHAN KUMAR

International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July ISSN BY B.MADHAN KUMAR International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July-2013 485 FLYING HOVER BIKE, A SMALL AERIAL VEHICLE FOR COMMERCIAL OR. SURVEYING PURPOSES BY B.MADHAN KUMAR Department

More information

Deployment and Drop Test for Inflatable Aeroshell for Atmospheric Entry Capsule with using Large Scientific Balloon

Deployment and Drop Test for Inflatable Aeroshell for Atmospheric Entry Capsule with using Large Scientific Balloon , Germany Deployment and Drop Test for Inflatable Aeroshell for Atmospheric Entry Capsule with using Large Scientific Balloon Kazuhiko Yamada, Takashi Abe (JAXA/ISAS) Kojiro Suzuki, Naohiko Honma, Yasunori

More information

Appenidix E: Freewing MAE UAV analysis

Appenidix E: Freewing MAE UAV analysis Appenidix E: Freewing MAE UAV analysis The vehicle summary is presented in the form of plots and descriptive text. Two alternative mission altitudes were analyzed and both meet the desired mission duration.

More information

General Dynamics F-16 Fighting Falcon

General Dynamics F-16 Fighting Falcon General Dynamics F-16 Fighting Falcon http://www.globalsecurity.org/military/systems/aircraft/images/f-16c-19990601-f-0073c-007.jpg Adam Entsminger David Gallagher Will Graf AOE 4124 4/21/04 1 Outline

More information

Management and Services Division Aircraft Technique Division Metalurgy Division Machine Shop and Tools Division

Management and Services Division Aircraft Technique Division Metalurgy Division Machine Shop and Tools Division PBS Velká Bíteš, a.s. (PBS) is a traditional producer of units and their parts for aerospace, power industry and transport. Today PBS employs about 800 people in four divisions: Management and Services

More information

SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM

SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM 25 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES SILENT SUPERSONIC TECHNOLOGY DEMONSTRATION PROGRAM Akira Murakami* *Japan Aerospace Exploration Agency Keywords: Supersonic, Flight experiment,

More information

Mega Engineering vehicles. the next generation of advanced apc

Mega Engineering vehicles. the next generation of advanced apc Mega Engineering vehicles the next generation of advanced apc Raptor Mega armored military vehicles is division of Mega Engineering Vehicles INC. Raptor the latest design by MEGA, the most advanced American

More information

Open & Evolutive UAV Architecture

Open & Evolutive UAV Architecture Open & Evolutive UAV Architecture 13th June UAV 2002 CEFIF 16-juin-02 Diapositive N 1 / 000 Report Documentation Page Form Approved OMB No. 0704-0188 Public reporting burden for the collection of information

More information

10th Australian International Aerospace Congress

10th Australian International Aerospace Congress AUSTRALIAN INTERNATIONAL AEROSPACE CONGRESS Paper presented at the 10th Australian International Aerospace Congress incorporating the 14th National Space Engineering Symposium 2003 29 July 1 August 2003

More information

AT-10 Electric/HF Hybrid VTOL UAS

AT-10 Electric/HF Hybrid VTOL UAS AT-10 Electric/HF Hybrid VTOL UAS Acuity Technologies Robert Clark bob@acuitytx.com Summary The AT-10 is a tactical size hybrid propulsion VTOL UAS with a nose camera mount and a large payload bay. Propulsion

More information

BAYLOR UNIVERSITY DEPARTMENT OF ENGINEERING. EGR 4347 Analysis and Design of Propulsion Systems Fall 2002 ASSIGNMENT GUIDELINES

BAYLOR UNIVERSITY DEPARTMENT OF ENGINEERING. EGR 4347 Analysis and Design of Propulsion Systems Fall 2002 ASSIGNMENT GUIDELINES BAYLOR UNIVERSITY DEPARTMENT OF ENGINEERING EGR 4347 Analysis and Design of Propulsion Systems Fall 2002 Design Project I Dr Van Treuren 100 points ASSIGNMENT GUIDELINES For this assignment, you may work

More information

German Aerospace Center Flight Operations

German Aerospace Center Flight Operations German Aerospace Center Flight Operations Introduction DLR is Germany s aerospace research center and space agency with about 4700 employees in 31 research institutes distributed over 8 main research centers

More information

Introduction. AeroJones Aviation Technology Co., Ltd.

Introduction. AeroJones Aviation Technology Co., Ltd. Contents 1. Introducing AeroJones 2. Business Concept 3. Operational Principle 4. Target Market 5. Technology Transfer 6. First Aircraft Testing 7. Product Introduction Introduction AeroJones Aviation

More information

Daher launches a new era of enhanced flight operations for TBM aircraft with the Me & My TBM smartphone app

Daher launches a new era of enhanced flight operations for TBM aircraft with the Me & My TBM smartphone app Press release Daher launches a new era of enhanced flight operations for TBM aircraft with the Me & My TBM smartphone app Friedrichshafen, Germany, April 18, 2018 TBM aircraft owners and operators were

More information

SURVEYOR-H. Technical Data. Max speed 120 km/h. Engine power 7.2 hp. Powerplant Modified Zenoah G29E. Fuel tank volume 3.6 l

SURVEYOR-H. Technical Data. Max speed 120 km/h. Engine power 7.2 hp. Powerplant Modified Zenoah G29E. Fuel tank volume 3.6 l rev. 28.10.14 * features & specifications are subject to change without notice. Technical Data Max speed 120 km/h Engine power 7.2 hp Powerplant Modified Zenoah G29E Fuel tank volume 3.6 l Payload with

More information

Selection of low-cost recovery system for Unmanned Aerial Vehicle

Selection of low-cost recovery system for Unmanned Aerial Vehicle Selection of low-cost recovery system for Unmanned Aerial Vehicle Abinaya.R 1, R. Arravind 2 1M.E Aeronautical Engineering, Department of Aeronautical Engineering, Nehru institute of Engineering and Technology,

More information

A brief History of Unmanned Aircraft

A brief History of Unmanned Aircraft A brief History of Unmanned Aircraft Technological Background Dr. Bérénice Mettler University of Minnesota Jan. 22-24, 2012 (v. 1/15/13) Dr. Bérénice Mettler (University of Minnesota) A brief History of

More information

Electric VTOL Aircraft

Electric VTOL Aircraft Electric VTOL Aircraft Subscale Prototyping Overview Francesco Giannini fgiannini@aurora.aero 1 08 June 8 th, 2017 Contents Intro to Aurora Motivation & approach for the full-scale vehicle Technical challenges

More information

31 st National Conference on FMFP, December 16-18, 2004, Jadavpur University, Kolkata

31 st National Conference on FMFP, December 16-18, 2004, Jadavpur University, Kolkata 31 st National Conference on FMFP, December 16-18, 24, Jadavpur University, Kolkata Experimental Characterization of Propulsion System for Mini Aerial Vehicle Kailash Kotwani *, S.K. Sane, Hemendra Arya,

More information

UNCLASSIFIED FY 2017 OCO. FY 2017 Base

UNCLASSIFIED FY 2017 OCO. FY 2017 Base Exhibit R-2, RDT&E Budget Item Justification: PB 2017 Air Force Date: February 2016 3600: Research, Development, Test & Evaluation, Air Force / BA 2: Applied Research COST ($ in Millions) Prior Years FY

More information

UNCLASSIFIED FY 2017 OCO. FY 2017 Base

UNCLASSIFIED FY 2017 OCO. FY 2017 Base Exhibit R-2, RDT&E Budget Item Justification: PB 2017 Air Force Date: February 2016 3600: Research, Development, Test & Evaluation, Air Force / BA 3: Advanced Technology Development (ATD) COST ($ in Millions)

More information

DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE

DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE ICAS 2002 CONGRESS DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE MUHAMMAD ASIM Engineering Wing PAF Base Minhas PAKISTAN,43175 a007pk@yahoo.com DR ABID ALI KHAN Aerospace Engg Dept College of Aeronautical

More information

ELECTRICAL SYSTEMS AIAA TEAM 1 VT AIAA TEAM 1 1

ELECTRICAL SYSTEMS AIAA TEAM 1 VT AIAA TEAM 1 1 ELECTRICAL SYSTEMS AIAA TEAM 1 VT AIAA TEAM 1 1 Electrical Systems in Aircraft Avionics Hydraulics Environmentalcontrol Lighting Subsystems VT AIAA TEAM 1 2 Electrical System Composition Batteries Alternators/Generators

More information

Landing Gear Layout Design for Unmanned Aerial Vehicle

Landing Gear Layout Design for Unmanned Aerial Vehicle Landing Gear Layout Design for Unmanned Aerial Vehicle Akhilesh Jha SDET Division, ADE/DRDO, Bangalore, India Corresponding author (email: akhilsdet@yahoo.com) Abstract Aircraft landing gear mechanism

More information

Electric Flight Potential and Limitations

Electric Flight Potential and Limitations Electric Flight Potential and Limitations Energy Efficient Aircraft Configurations, Technologies and Concepts of Operation, Sao José dos Campos, 19 21 November 2013 Dr. Martin Hepperle DLR Institute of

More information

All in One Weapons QRL (Quick Reference List)

All in One Weapons QRL (Quick Reference List) All in One Weapons QRL (Quick Reference List) Nomenclature Max Range miles AIM 120 25 a/c launch and leave / Radar guided AIM 7 15 a/c must maintain lock / Radar guided AIM 9 M 10 a/c all aspect IR SRM

More information

JSBSim Library for Flight Dynamics Modelling of a mini-uav

JSBSim Library for Flight Dynamics Modelling of a mini-uav JSBSim Library for Flight Dynamics Modelling of a mini-uav Tomáš Vogeltanz and Roman Jašek Tomas Bata University in Zlín, Faculty of Applied Informatics Department of Informatics and Artificial Intelligence

More information

Overview. Mission Overview Payload and Subsystems Rocket and Subsystems Management

Overview. Mission Overview Payload and Subsystems Rocket and Subsystems Management MIT ROCKET TEAM Overview Mission Overview Payload and Subsystems Rocket and Subsystems Management Purpose and Mission Statement Our Mission: Use a rocket to rapidly deploy a UAV capable of completing search

More information

Deployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon

Deployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon 1 Deployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon Kazuhiko Yamada, Takashi Abe (JAXA/ISAS) Kojiro Suzuki, Naohiko Honma, Yasunori Nagata, Masashi Koyama (The

More information

Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials. Ripley Valley Rural Fire Brigade - August 2010

Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials. Ripley Valley Rural Fire Brigade - August 2010 Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials Ripley Valley Rural Fire Brigade - August 2010 The Brigade offered to help evaluate the capabilities of an Unmanned Aerial Vehicle (UAV)

More information

DEVELOPMENT OF A MORPHING FLYING PLATFORM FOR ADAPTIVE CONTROL SYSTEM STUDY

DEVELOPMENT OF A MORPHING FLYING PLATFORM FOR ADAPTIVE CONTROL SYSTEM STUDY 27 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES DEVELOPMENT OF A MORPHING FLYING PLATFORM FOR ADAPTIVE CONTROL SYSTEM STUDY Taufiq Mulyanto, M. Luthfi I. Nurhakim, Rianto A. Sasongko Faculty

More information

SKYRANGER OA-X2 LIGHT-ATTACK AIRCRAFT 27 July 2017

SKYRANGER OA-X2 LIGHT-ATTACK AIRCRAFT 27 July 2017 SKYRANGER OA-X2 LIGHT-ATTACK AIRCRAFT 27 July 2017 Puma Aero Marines Skyranger OA-X2 is to perform light attack, armed reconnaissance, counter-insurgency (COIN) and military flight trainer, available at

More information

SPECIAL MISSION AIRCRAFT

SPECIAL MISSION AIRCRAFT SPECIAL MISSION AIRCRAFT precision from above FACTS AND SPECIFICATIONS DA42 MPP Guardian - Facts and Specifications Power plant Engine Propeller Fuel grades 2x AUSTRO ENGINE AE300 (168 hp, turbo charged)

More information

INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI

INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI INVESTIGATION OF ICING EFFECTS ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT AT TSAGI Andreev G.T., Bogatyrev V.V. Central AeroHydrodynamic Institute (TsAGI) Abstract Investigation of icing effects on aerodynamic

More information

A high-glide ram-air parachute for 6,000 kg payloads, tested with the FASTWing CL test-vehicle.

A high-glide ram-air parachute for 6,000 kg payloads, tested with the FASTWing CL test-vehicle. 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar 4-7 May 2009, Seattle, Washington AIAA 2009-2933 A high-glide ram-air parachute for 6,000 kg payloads, tested with the FASTWing

More information

Overview of BAE Systems Regional Aircraft

Overview of BAE Systems Regional Aircraft Overview of BAE Systems Regional Aircraft Dr Mike West Chief Technologist Introduction to BAE Systems Regional Aircraft Eurofighter /Typhoon Joint Strike Fighter Nimrod MRA4 Surface Ships Customer Solutions

More information

UAV Drones. Team RamRod: Tyler Barry James Bohn Daniel Ramirez Hari Shrestha Arlo Swanson Garret Wilbanks

UAV Drones. Team RamRod: Tyler Barry James Bohn Daniel Ramirez Hari Shrestha Arlo Swanson Garret Wilbanks UAV Drones Team RamRod: Tyler Barry James Bohn Daniel Ramirez Hari Shrestha Arlo Swanson Garret Wilbanks Outline Introduction History Technology and Applications Current Future Economics and Marketability

More information

UAV Systems Comparison. Planes, Frames and Autopilots

UAV Systems Comparison. Planes, Frames and Autopilots UAV Systems Comparison Planes, Frames and Autopilots Presenter: Robert Lefebvre BASc Mechanical Engineering, University of Ottawa Managing Director NOVAerial Robotics Inc. Ardupilot Developer 6 Years UAV

More information

UNCLASSIFIED R-1 ITEM NOMENCLATURE

UNCLASSIFIED R-1 ITEM NOMENCLATURE Exhibit R-2, RDT&E Budget Item Justification: PB 213 Navy DATE: February 212 COST ($ in Millions) FY 211 FY 212 FY 214 FY 215 FY 216 FY 217 To Program Element 67.48 18.248 99.6-99.6 49.2 12.2 13.4 -. 349.696

More information

Content. Introduction. Technology. Type of unmanned vehicle. Past, Present, Future. Conclusion

Content. Introduction. Technology. Type of unmanned vehicle. Past, Present, Future. Conclusion Introduction Content Technology Type of unmanned vehicle Past, Present, Future Conclusion What is unmanned vehicles? l Without a person on board l Remote controlled l Remote guided vehicles Reduce casualty

More information

A VERY UNIQUE UAV FLAMINGO MK1 UAV Silvertone Electronics Australia

A VERY UNIQUE UAV FLAMINGO MK1 UAV Silvertone Electronics Australia A VERY UNIQUE UAV FLAMINGO MK1 UAV 01 DESIGN BACKGROUND The design was born out of a perceived need for a low capital cost, surveillance tool for large Farm/ Property owners. 02 SIZE AND WEIGHT The size,

More information

How the V-22 Osprey Works

How the V-22 Osprey Works How the V-22 Osprey Works It has long been a dream of aircraft designers to create an airplane that not only can fly long ranges at high speeds and carry heavy cargo, but can also take off, hover and land

More information

THE FALCON REDUNDANCY HIGH WIND TOLERANCE BEST USED FOR SURVEILLANCE & SECURITY DELIVERY & TRANSPORT

THE FALCON REDUNDANCY HIGH WIND TOLERANCE BEST USED FOR SURVEILLANCE & SECURITY DELIVERY & TRANSPORT THE FALCON REDUNDANCY HIGH WIND TOLERANCE The Falcon's new air frame and motor configuration is the new best in its class of light payloads with flight times of up to 50 minutes. This makes the Falcon

More information

Application of Airbag Technology for Vehicle Protection

Application of Airbag Technology for Vehicle Protection Application of Airbag Technology for Vehicle Protection Richard Fong, William Ng, Peter Rottinger and Steve Tang* U.S. ARMY ARDEC Picatinny, NJ 07806 ABSTRACT The Warheads Group at the U.S. Army ARDEC

More information

Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration

Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration 1 Methodology for Distributed Electric Propulsion Aircraft Control Development with Simulation and Flight Demonstration Presented by: Jeff Freeman Empirical Systems Aerospace, Inc. jeff.freeman@esaero.com,

More information

Contents. BAE SYSTEMS PROPRIETARY Internal UNCLASSIFIED Use Only Unpublished Work Copyright 2013 BAE Systems. All rights reserved.

Contents. BAE SYSTEMS PROPRIETARY Internal UNCLASSIFIED Use Only Unpublished Work Copyright 2013 BAE Systems. All rights reserved. Contents Aim of presentation. Who do we interface with. What does safe separation entail. What do we class as a store. Why is there a need for safe separation analysis. Methods for performing safe separation

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design Tables No Component Primary function Major areas of influence 1 Fuselage Payload accommodations

More information

H125. HELICOPTERS Civil

H125. HELICOPTERS Civil H125 HELICOPTERS Civil 002 H125 Ready for any mission with the capability to : - Transport safely and comfortably up to 6 passengers + pilot - Sling 1,400 kg load - Several hundreds STC exist around the

More information

Star Tower. Why Aerostats Star Tower: Applications Summary. Description Performance Features Payload. Product CARAVAN INTERNATIONAL CORPORATION

Star Tower. Why Aerostats Star Tower: Applications Summary. Description Performance Features Payload. Product CARAVAN INTERNATIONAL CORPORATION AEROSTATS CARAVAN INTERNATIONAL CORPORATION Star Tower Why Aerostats Star Tower: Product Description Performance Features Payload Applications Summary Why Our Aerostats Provide persistent wide-area coverage

More information

Aermacchi M-345 THE NEXT GENERATION TRAINER

Aermacchi M-345 THE NEXT GENERATION TRAINER Aermacchi M-345 THE NEXT GENERATION TRAINER Aermacchi M-345 THE NEXT GENERATION TRAINER The new Aermacchi M-345 is the latest-generation training platform from Leonardo Aircraft, ideally-suited for the

More information

Analysts/Fund Managers Visit 19 April Autonomous Systems and Future Capability Mark Kane

Analysts/Fund Managers Visit 19 April Autonomous Systems and Future Capability Mark Kane Analysts/Fund Managers Visit 19 April 2007 Autonomous Systems and Future Capability Mark Kane The Rationale for UAVs The Rationale for UAVs UAVs generally seen to carry out the dull, dirty, and dangerous

More information

PAC 750XL PAC 750XL PAC-750XL

PAC 750XL PAC 750XL PAC-750XL PAC 750XL The PAC 750XL combines a short take off and landing performance with a large load carrying capability. The PAC 750XL is a distinctive type. Its design philosophy is reflected in the aircraft's

More information

Development of an Extended Range, Large Caliber, Modular Payload Projectile

Development of an Extended Range, Large Caliber, Modular Payload Projectile 1 Development of an Extended Range, Large Caliber, Modular Payload Projectile April 12th, 2011 Miami, Florida, USA 46 th Annual Gun & Missile Systems Conference & Exhibition Speaker: Pierre-Antoine Rainville

More information

FLIGHT READINESS REVIEW TEAM OPTICS

FLIGHT READINESS REVIEW TEAM OPTICS FLIGHT READINESS REVIEW TEAM OPTICS LAUNCH VEHICLE AND PAYLOAD DESIGN AND DIMENSIONS Vehicle Diameter 4 Upper Airframe Length 40 Lower Airframe Length 46 Coupler Band Length 1.5 Coupler Length 12 Nose

More information

German Aerospace Center Flight Operations

German Aerospace Center Flight Operations German Aerospace Center Flight Operations Introduction DLR is Germany s aerospace research center and space agency with about 4700 employees in 31 research institutes distributed over 8 main research centers

More information

Exhibit R-2, RDT&E Budget Item Justification

Exhibit R-2, RDT&E Budget Item Justification PE NUMBER: 0305219F PE TITLE: PREDATOR Exhibit R-2, RDT&E Budget Item Justification BUDGET ACTIVITY PE NUMBER AND TITLE Cost ($ in Millions) FY 2008 FY 2009 FY 2010 FY 2011 FY 2012 FY 2013 FY 2014 FY 2015

More information

Cable Dragging Horizontal Takeoff Spacecraft Air Launch System

Cable Dragging Horizontal Takeoff Spacecraft Air Launch System Cable Dragging Horizontal Takeoff Spacecraft Air Launch System Author: Zhixian Lin December 31, 2017 i Contents Abstract...ii 1. Cable Dragging Horizontal Takeoff Spacecraft Air Launch System... 1 2. The

More information

Instruction Manual. Twin 70MM EDF

Instruction Manual. Twin 70MM EDF Instruction Manual NOTE : SKY FLIGHT HOBBY CO., LTD will not take any responsibility for damage or accident caused by the improper use of this model. Twin 70MM EDF WARNING MiG-29 Fighter Jet is an Electric

More information

Design and Simulation of New Versions of Tube Launched UAV

Design and Simulation of New Versions of Tube Launched UAV 21st International Congress on Modelling and Simulation, Gold Coast, Australia, 29 Nov to 4 Dec 2015 www.mssanz.org.au/modsim2015 Design and Simulation of New Versions of Tube Launched UAV Y. Zhou and

More information

AW139M SIMPLY NO RIVALS

AW139M SIMPLY NO RIVALS AW139M SIMPLY NO RIVALS DELIVERING CAPABILITY FOR DEMANDING MISSIONS The AW139M is the militarised version of the AW139, a new generation intermediate twin-turbine helicopter that sets the standard against

More information

3 rd EASN Association International Workshop on AeroStructures

3 rd EASN Association International Workshop on AeroStructures 3 rd EASN Association International Workshop on AeroStructures ESTOLAS PROJECT Analysis of the design features and flying -technical characteristics of the ESTOLAS hybrid aircraft prototype Speaker Vladimir

More information

PROJECT HAVE DOUGHNUT -

PROJECT HAVE DOUGHNUT - Foreign Technology Division PROJECT HAVE DOUGHNUT - EXPLOITATION OF THE MIG-21 Rob Young Historian National Air and Space Intelligence Center This Briefing is Classified: UNCLASSIFIED//APPROVED FOR PUBLIC

More information

SpaceLoft XL Sub-Orbital Launch Vehicle

SpaceLoft XL Sub-Orbital Launch Vehicle SpaceLoft XL Sub-Orbital Launch Vehicle The SpaceLoft XL is UP Aerospace s workhorse space launch vehicle -- ideal for significant-size payloads and multiple, simultaneous-customer operations. SpaceLoft

More information

DESIGN AND DEVELOPMENT OF A MICRO AIR VEHICLE (µav) CONCEPT: PROJECT BIDULE

DESIGN AND DEVELOPMENT OF A MICRO AIR VEHICLE (µav) CONCEPT: PROJECT BIDULE DESIGN AND DEVELOPMENT OF A MICRO AIR VEHIE (µav) CONCEPT: PROJECT BIDULE Mr T. Spoerry, Dr K.C. Wong School of Aerospace, Mechanical and Mechatronic Engineering University of Sydney NSW 6 Abstract This

More information

The winner team will have the opportunity to perform a wind tunnel test campaign in the transonic/supersonic Wind tunnel at the VKI.

The winner team will have the opportunity to perform a wind tunnel test campaign in the transonic/supersonic Wind tunnel at the VKI. Aircraft Design Competition Request for proposal (RFP) - High speed UAV Objectives: This RFP asks for an original UAV design capable of reaching, in less than 15 minutes, a given target located at 150

More information