DOCSLIB.ORG

UAV CHART 2011 Low-Res

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text

Load more

20112011 WorldwideWorldwide UAVUAV RoundupRoundup Country Prime Designation Development Production Operation Propulsion Gross Wt., kg Payload Wt., kg Wing Span, m Endurance, hr Range, km Ceiling, m Mission Country Prime Designation Development Production Operation Propulsion Gross Wt. kg Payload Wt., kg Wing Span, m Endurance , hr Range, km Ceiling, m Mission ABU DHABI ADCOM Military Industries Yabhon RX-6 Completed (?) In production Deployed Piston pusher prop 1,100 110 6 30 14,500 R/S RUSSIA (continued) ZALA 421-09 Under way Piston prop 70 10 3.9 10.5 50 3,000 RSTA - BDA -satcomm Yabhon RX-18 Under way Jet 1,250 18 Predator-class MALE ZALA 421-12 MAV Completed Electric C-L 3.9 1 1.6 2 3,600 R/S - monitoring (ADCOM uses the Yabhon Yabhon HMD Completed In production Deployed Twin turbo 1.2 High-speed target drone ZALA 421-15 VTOL Under way Electric 5 0.5 Rotor diam. 1.35 20 min 15 2,500 R/S - monitoring name for a wide range of UAVs Yabhon HM Completed In production Deployed Turbine ZALA 421-16 Completed Piston prop - C-L 16 3 1.62 7 50 3,000 R/S - SAR - video relay; monitoring with little else in common) Yabhon-H Completed In production Deployed Piston pusher prop 3.28 8 Reconnaissance ZALA 421-20 (?) GAS 200 50 6 8 70-400 3,700 Reconnaissance/surveillance; monitoring Yabhon-M Completed In production Deployed 30 5.7 Reconnaissance ZALA 421-21 mini-VTOL (?) Electric - 6 rotors 1.5 0.5 Rotor diam. 0.22 25 min 5 1,000 Surveillance; monitor; video Yabhon-R Completed In production Deployed 50 6.56 30 MALE R/S; SAR; monitoring ZALA 421-23 VTOL Under way GAS rotor 35 13 Rotor diam. 2.15 1.5 40 3,000 Monitoring; video SAT-400 Completed In production Deployed Pusher prop 85 2.75 2 Target drone Eniks E85 Under way On request Pulse jet 140 2 43.5 mi 9,850 Target drone Smart Eye Under way HALE - Predator-class E95 Under way Pulse jet 60 2.4 0.5 116 mi 10,000 Target drone ARGENTINA Argentine Air Force Proyecto UAV Etapa 1 Under way 300 50 8 R90 Under way Pulse jet 45 2.6 0.5 36 mi 10,000 Tactical reconnaissance Proyecto UAV Etapa 2 15 T23 Eleron Under way Electric - H-L 3 1.4 1 6.5 mi 2,000 Aerial photography; monitoring Proyecto UAV Etapa 3 3 months HALE Irkut DA42 Under way Twin piston 350 Argentine Army Lipan M3 Under way 60 20 40 Irkut-2M Completed Under way Electric - H-L 3 1.5 1.5 9,900 Multimission Argentine Navy Guardian Under way 80 30 50 Irkut-10 Completed Under way Electric - H-L 8.5 5.7 2.5 9,900 Multimission Nostromo Defensa Cabure III Completed Deployed Electric 3.5 1.7 1.2 10 LOS 2,000 RSTA - BDA Multipurpose UAS Under way Pusher prop 440 110 19.5 12 720 19,000 Yarará Under way Limited Deployed Piston 30 7 3.98 6 50 3,000 R/S - BP Kamov Ka-137 VTOL Under way Piston 280 176 4 16,400 CBW sning, border/sheries/ecol monitor Yagua Status unknown No longer on website Piston/electric pusher prop 12 2 2.7 16 piston/1.5 elect. 30+ Originally planned as TUAV for special ops MBVK-137 VTOL Under way Piston 280 50-80 Rotor diam. 5.3 4 530 5,000 Based on Ka-137 AUSTRALIA Aerosonde (division of AAI) Aerosonde SUAS Completed In production Deployed GAS pusher prop 15 5.4 2.9 30 1,609 6,096 ISR; jamming Iskatel Design Bureau Voron BAE Systems Kingsher Completed Research prototype Piston pusher prop 60 15 4.13 4.5 50 Demonstrator Luch Design Bureau Tipchak Under way Limited 60 3.5 70-120 Reconnaissance Kingsher Mk2 Completed Full production Deployed Pusher prop 115 30 4.23 15 Demonstrator Mikoyan Skat (Manta Ray) UCAV RDT&E 1 Klimov RD-5000B turbofan 10,000 2,000 11.5 2,000 SEAD Kalkura Completed Full production Deployed Turbojet 662 3.02 2 12,192 Target drone NII Kulon Filin Under way Turbojet 3,000 1 310 19,500 ft Tactical reconnaissance (w/Univ. of Sydney) Brumby Mk3 Completed 45 7 2.82 2 Demonstrator Moskit Under way 290 1.5 83 11,500 ft Tactical reconnaissance Codarra Advanced Systems Avatar P2 Completed Full production Deployed Electric prop - H-L 5.5 1 2.55 1 10 305 R/S - monitoring Novik 21st Century Brat Under way CSIRO RUA VTOL Completed Testing Gas rotor 5 Rotor diam. 1.8 Test and demonstration Grant Under way Silvertone Flamingo Mk 2 (single boom) Under way Deployed Pusher prop 20 10 4 7 UAV training B Sukhoi BAS-62 Under way Jet 16,000 lb 24 63,000 ft Global Hawk-class R/S Strella Production Assoc. M-932 Dan Under way Turbojet 345 2.7 40 min 29,500 ft Target UAV Vision G18 Aeolus Completed Gas rotor 14 5 Rotor diam. 1.8 3 100 Monitoring Sukhoi Zond-1 Under way Twin jet 12,000 1,500 35 18 16,000 ATC comm relay T21 Completed Microjet turbine 30 Rotor diam. 2.1 1.5 Monitoring Zond-2 Under way Twin jet 12,000 1,500 35 24 16,000 Multispectral monitoring AUSTRIA Schiebel CAMCOPTER S-100 Completed In production (?) Worldwide 50 HP rotary engine 110 50 Main rotor diam. 3.4 6 or 10+ 80 or 180 Up to 6,000 Zond-3M Under way Turbofan pusher prop 2,000 500 16 12 8,000 Multispectral monitoring BELGIUM Flying-Cam Flying-Cam III E-SARAH Completed Deployed Electric rotor 25 Tupolev BAK-SD candidate Under way 500-700 MALE - RSTA - strike BRAZIL Aeroeletrônica Ltd. - Elbit subsidiary Hermes 450 Completed Piston pusher prop 450 150 10.5 20 120 LOS 5,486 R/S, BDA Tu-143 Upgrading Deployed 1,230 13 min 180-360 2,000 BELARUS Kvand Ventures Husky Completed Twin turbojet rotor 90 42 Rotor diam. 3.2 1.2 60 1,800 S/SAR helicopter Tu-243 REIS2000-D Upgrading Deployed Turbojet - RATO 1,451.50 200 2.24 360 2,000/5,000 Recon - low-altitude attack CANADA Aeryon Labs Scout VTOL MAV Completed Limited Limited Electric - 4 rotor 1.7 250 g 80 cm diam. 20 min 3 333 R/S - SAR Transas Dozor-100 Under way Testing Piston pusher prop 95 10 400 Reconnaissance/surveillance Dragany Innovations Draganyer X4 Completed Since 2009 Deployed Electric - MAV 0.98 0.25 Rotor diam. 0.78 0.3 SR < 1 10-200 ImiNT, IR, R/S, S&R, TUAV Dozor-600 Under way Testing Piston pusher prop 640 120 12 24 900 7,500 R/S - comm relay Draganyer X6 Completed Since 2008 Deployed Electric - MAV 1.5 0.5 Rotor diam. 0.99 0.3 SR < 1 200 ImiNT, IR, R/S, S&R, TUAV Vega Aist (Stork) Under way Testing Twin piston prop - A-L 600 13.8 (?) 12 250 6,000 R/S Draganyer X8 Completed Begins 2011 Testing Electric - MAV 2.7 1 Rotor diam. 1.06 0.3 SR < 1 200-300 ImiNT, IR, R/S, S&R, TUAV Yakovlev PCHELA-1T 1970s-1980s Limited Piston 140 3.3 2 36 8,200 R/S - daytime TV camera MMIST SnowGoose CQ-10A Completed Under way Deployed Turboprop parafoil or Rotor VTOL 260.8 15 w/100 lb ISR, comm; cargo Albatros VTOL Under way Tilt rotor 450 26 7 110 350 R/S - SAR - civil ecological/counter-drug/border patrol SnowGoose CQ-10B VTOL Under way Limited Limited Turbo pusher prop/rotor 227 24 150 Near-VTOL - force protection; small unit resupply Strekoza/Expert Under way Pusher prop - C-L 40 6 60 450 R/S - SAR microPilot CropCam Completed Limited Battery - H-L 2.72 2.4 20 min 670 Ag/environmental monitor Pchela-1K Modernization Under way Deployed Pusher prop - T-L 300 10.5 3.5 36 11,500 day/night R/S - low-light TV camera MP-Trainer Completed Gas prop 2.95 0.9 1.75 20 min 4 Trainer - testing Pchela-e/Shmel-2 Under way C-L 485 6 R/S - electronic countermeasures MP-Vision Completed Battery - H-L 2.72 0.45 2.4 55 min Photo SINGAPORE Singapore Technology Aerospace Fantail 5000 Under way Ducted fan VTOL 6.5 0.9 Rotor diam. 46 cm. 0.5 8 914 RSTA - BDA - Photo CHILE IDETEC Sirol Completed Electric prop 3 3.8 2-4 Demonstrator SkyBlade III Under way Electric - prop 5 2.6 1 8 460 RSTA/BDA Stardust II Completed Electric prop 3 3.1 0.66 Agriculture; surveillance SkyBlade IV Under way Pusher prop - C-L 70 12 3.7 100 4,572 RSTA/SAR Javelin-X Completed Gas prop - CL 24 3.4 1 Aerial target SOUTH AFRICA Advanced Technologies Kiwit MUAV Under way Electric - H-L 6.5 1.8 1 3 495 Mini-UAV RMS SA Mantarraya Completed Battery - prop - CL 60 15 2.52 4 100 3,000 Reconnaissance; comms relay & Engineering Roadrunner Under way 6 1 1.5 1 R/S - aerial pursuit Petre II Completed Turbine - JATO 183.4 31 1.69 1 100 12,000 Aerial target Sentinel 500 m Under way C-L 150 5 5 Trauco III Completed Battery - prop - CL 210 20 4.02 55 min 100 8,200 Aerial target Sentinel 620 Under way 200 35 6.2 12 CHINA * ASN Technology Group ASN-211 MUAV In development Flapping wings 220 g 200 Low-altitude reconnaissance Sentinel 800 Under way 250 35 8 20 ASN-213 morphing Under way Folding wings 5 1 0.632 Unclear; morphing wing has been linked to fast attack Vigil EE Under way Pusher prop 80 20 4 8 Low-cost civilian UAV ASN-229A In development IOC 2011(?) 800 100, plus sensors 20 2,000 10,000 Reconnaissance and precise attack Vigil SR Under way Pusher prop 40 10 4 4 Low-cost civilian UAV ASN-106 In development Jet 170 20 1 High-speed target drone Vulture Completed In production Deployed Piston - Pusher prop 100 25 5.2 125 mi 16,400 TUAV - R/S - EW ASN-9 (Ba-9) Completed Deployed Prop 2.82 1 Ship-launched target drone Super Vulture II Under way Under way Piston - heavy fuel 125 25 5.2 3 80-200 16,400 RSTA - BDA ASN-15 Completed Deployed Piston H-L 6.5 3 1 10 1,625 ISR Council for Scientic & Industrial Res.
Recommended publications
  • Turbulence in the Gulf

    Turbulence in the Gulf

    Come and see us at the Dubai Airshow on Stand 2018 AEROSPACE November 2017 FLYING FOR THE DARK SIDE IS MARS GETTING ANY CLOSER? HYBRID-ELECTRIC PROPULSION www.aerosociety.com November 2017 Volume 44 Number 11 Volume TURBULENCE IN THE GULF SUPERCONNECTOR AIRLINES BATTLE HEADWINDS Royal Aeronautical Society Royal Aeronautical N EC Volume 44 Number 11 November 2017 Turbulence in Is Mars getting any 14 the Gulf closer? How local politics Sarah Cruddas and longer-range assesses the latest aircraft may 18 push for a human impact Middle mission to the Red East carriers. Planet. Are we any Contents Clément Alloing Martin Lockheed nearer today? Correspondence on all aerospace matters is welcome at: The Editor, AEROSPACE, No.4 Hamilton Place, London W1J 7BQ, UK [email protected] Comment Regulars 4 Radome 12 Transmission The latest aviation and Your letters, emails, tweets aeronautical intelligence, and feedback. analysis and comment. 58 The Last Word Short-circuiting electric flight 10 Antenna Keith Hayward considers the Howard Wheeldon looks at the current export tariff spat over MoD’s planned Air Support to the Bombardier CSeries. Can a UK low-cost airline and a US start-up bring electric, green airline travel Defence Operational Training into service in the next decade? On 27 September easyJet revealed it had (ASDOT) programme. partnered with Wright Electric to help develop a short-haul all-electric airliner – with the goal of bringing it into service within ten years. If realised, this would represent a game-changing leap for aviation and a huge victory for aerospace Features Cobham in meeting or even exceeding its sustainable goals.
  • Flying High One Year on from Lifting Off Contents

    Flying High One Year on from Lifting Off Contents

    Aerospace Growth Partnership FLYING HIGH ONE YEAR ON FROM LIFTING OFF CONTENTS 4 Forewords 6 Summary 10 Market Forecast in Civil Aerospace 12 Importance of Aerospace to the UK 16 AGP Timeline Since Lifting Off 18 Technology 22 Supply Chain Competitiveness & Manufacturing Capability 26 Skills 30 Where Next? 2 3 FOREWORDS CONTINUED INDUSTRY COMMITMENT TO AGP When we started on the AGP journey, our main objectives were to create This report outlines the excellent progress made under the Aerospace Growth Partnership and the plan for moving forward. a partnership between Government, industry and academia and develop a strategy that continued to secure the UK’s position as a leading aerospace The UK aerospace industry will continue to work with Government and academia to implement the aerospace industrial strategy and nation. I am delighted to say, not only have we achieved those objectives, but ensure it meets the objectives of creating long-term growth, wealth and skilled jobs for the nation. we are continually setting the bar higher. This document provides an update on those achievements over the last twelve months and sets out the game plan going forward. AGP is timely, we find ourselves in an aerospace “super cycle” and the opportunities over the next twenty-five years are just getting bigger. AGP will continue to ensure that UK industry is targeting the right customers and markets with the right technology, skills, capability and products. These are incredibly exciting times for UK aerospace and I am delighted that AGP Marcus Bryson CBE, has acted as a unifying force in bringing together senior executives, key AGP Co-Chair influencers and decision makers to form a dynamic team.
  • Aircraft of Today. Aerospace Education I

    Aircraft of Today. Aerospace Education I

    DOCUMENT RESUME ED 068 287 SE 014 551 AUTHOR Sayler, D. S. TITLE Aircraft of Today. Aerospace EducationI. INSTITUTION Air Univ.,, Maxwell AFB, Ala. JuniorReserve Office Training Corps. SPONS AGENCY Department of Defense, Washington, D.C. PUB DATE 71 NOTE 179p. EDRS PRICE MF-$0.65 HC-$6.58 DESCRIPTORS *Aerospace Education; *Aerospace Technology; Instruction; National Defense; *PhysicalSciences; *Resource Materials; Supplementary Textbooks; *Textbooks ABSTRACT This textbook gives a brief idea aboutthe modern aircraft used in defense and forcommercial purposes. Aerospace technology in its present form has developedalong certain basic principles of aerodynamic forces. Differentparts in an airplane have different functions to balance theaircraft in air, provide a thrust, and control the general mechanisms.Profusely illustrated descriptions provide a picture of whatkinds of aircraft are used for cargo, passenger travel, bombing, and supersonicflights. Propulsion principles and descriptions of differentkinds of engines are quite helpful. At the end of each chapter,new terminology is listed. The book is not available on the market andis to be used only in the Air Force ROTC program. (PS) SC AEROSPACE EDUCATION I U S DEPARTMENT OF HEALTH. EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRO OUCH) EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIG INATING IT POINTS OF VIEW OR OPIN 'IONS STATED 00 NOT NECESSARILY REPRESENT OFFICIAL OFFICE OF EOU CATION POSITION OR POLICY AIR FORCE JUNIOR ROTC MR,UNIVERS17/14AXWELL MR FORCEBASE, ALABAMA Aerospace Education I Aircraft of Today D. S. Sayler Academic Publications Division 3825th Support Group (Academic) AIR FORCE JUNIOR ROTC AIR UNIVERSITY MAXWELL AIR FORCE BASE, ALABAMA 2 1971 Thispublication has been reviewed and approvedby competent personnel of the preparing command in accordance with current directiveson doctrine, policy, essentiality, propriety, and quality.
  • Leading the Charge How Air Race E Plans to Put Electric Aviation on the Map

    Leading the Charge How Air Race E Plans to Put Electric Aviation on the Map

    160 years of innovation theengineer.co.uk May 2019 | £3.70 Leading the charge How Air Race E plans to put electric aviation on the map Advanced Manufacturing News, comment and in-depth analysis from Future threats Home help Car of the issue the world of production technology BAE’s technology director on Inside the centre developing The Jaguar F-Pace SVR, a luxury innovating in an increasingly technology to help those SUV that offers other- dangerous world »24 living with dementia »30 worldly performance »32 » 37 Cover_The Engineer - May 2019_The Engineer 1 07/05/2019 14:20 BOTH COME WITH for 3TRAINING peopleFREE over 3 days. XYZ UMC 4+1 XYZ UMC-5X FROM £129 DIRECT DRIVE ,915 HIGH TORQUE MOTOR DIRECT DRIVE +VAT HIGH TORQUE MOTOR FROM 5 axis NO90 WORM OR WHEELRPM NO90 WORM OR WHEELRPM £149,625 (4+1) multi face or +VAT 5 axis simultaneous ? Stay ahead of the pack with either full blown simultaneuos 5 axis or 5 axis via 4+1. n Side-mounted 24, 30, 48 or 60 tools ATC for quick tool changing. Call today Many companies don’t actually use 5 axis simultaneous, the complexity means CAD/CAM is essential to write and for the full n Linear scales X Y and Z (optional on XYZ UMC 4+1). develop these complex components, but multi-face machining can save hours of time even on simple jobs that are technical 12 page currently done on a 3 axis VMC, to machine 6 sides of a dice requires 6 set ups on a VMC and 2 on a Multi-face machine.
  • FAA Order JO 7110.65U, Air Traffic Control

    FAA Order JO 7110.65U, Air Traffic Control

    ORDER JO 7110.65U Air Traffic Organization Policy Effective Date: February 9, 2012 SUBJ: Air Traffic Control This order prescribes air traffic control procedures and phraseology for use by personnel providing air traffic control services. Controllers are required to be familiar with the provisions of this order that pertain to their operational responsibilities and to exercise their best judgment if they encounter situations not covered by it. Distribution: ZAT-710, ZAT-464 Initiated By: AJV-0 Vice President, System Operations Services RECORD OF CHANGES DIRECTIVE NO. JO 7110.65U CHANGE SUPPLEMENTS CHANGE SUPPLEMENTS TO OPTIONAL TO OPTIONAL BASIC BASIC FAA Form 1320−5 (6−80) USE PREVIOUS EDITION 2/9/12 JO 7110.65U Explanation of Changes Basic Direct questions through appropriate facility/service center office staff to the Office of Primary Interest (OPI) a. 2−5−2. NAVAID TERMS d. 5−9−10. SIMULTANEOUS INDEPEND- 4−2−1. CLEARANCE ITEMS ENT APPROACHES TO WIDELY-SPACED 4−2−5. ROUTE OR ALTITUDE PARALLEL RUNWAYS WITHOUT FINAL AMENDMENTS MONITORS 4−2−9. CLEARANCE ITEMS 4−3−2. DEPARTURE CLEARANCE This change adds a new paragraph allowing 4−3−3. ABBREVIATED DEPARTURE simultaneous independent approaches to widely CLEARANCE spaced parallel runways separated by 9,000 feet or 4−7−1. CLEARANCE INFORMATION more−without monitors. This change cancels and 4−8−2. CLEARANCE LIMIT incorporates N JO 7110.559, Simultaneous Inde- This change clarifies how to issue clearances that pendent Approaches to Widely-Spaced Parallel contain NAVAIDs and provides new phraseology Runways Without Final Monitors, effective and examples. July 29, 2011. b.
  • FINAL PROGRAM #Aiaascitech

    FINAL PROGRAM #Aiaascitech

    4–8 JANUARY 2016 SAN DIEGO, CA The Largest Event for Aerospace Research, Development, and Technology FINAL PROGRAM www.aiaa-SciTech.org #aiaaSciTech 16-928 WHAT’S IMPOSSIBLE TODAY WON’T BE TOMORROW. AT LOCKHEED MARTIN, WE’RE ENGINEERING A BETTER TOMORROW. We are partnering with our customers to accelerate manufacturing innovation from the laboratory to production. We push the limits in additive manufacturing, advanced materials, digital manufacturing and next generation electronics. Whether it is solving a global crisis like the need for clean drinking water or travelling even deeper into space, advanced manufacturing is opening the doors to the next great human revolution. Learn more at lockheedmartin.com © 2014 LOCKHEED MARTIN CORPORATION VC377_164 Executive Steering Committee AIAA SciTech 2016 2O16 Welcome Welcome to the AIAA Science and Technology Forum and Exposition 2016 (AIAA SciTech 2016) – the world’s largest event for aerospace research, development, and technology. We are confident that you will come away from San Diego inspired and with the tools necessary to continue shaping the future of aerospace in new and exciting ways. From hearing preeminent industry thought leaders, to attending sessions where cutting- edge research will be unveiled, to interacting with peers – this will be a most fulfilling week! Our organizing committee has worked hard over the past year to ensure that our plenary sessions examine the most critical issues facing aerospace today, such as aerospace science and Richard George Lesieutre technology policy, lessons learned from a half century of aerospace innovation, resilient design, Christiansen The Pennsylvania and unmanned aerial systems. We will also focus on how AIAA and other stakeholders in State University Sierra Lobo, Inc.
  • Table of Contents Next Page

    Table of Contents Next Page

    , SERVICE PUBLICATION OF OCKHEED-GEORGIA COMPANY / DIVISION OF OCKHEED CORPORATION Editor: Don H. Hungate Associate Editors: Charles I. Gale, James A. Loftin, Arch McCleskey, Patricia Thomas Art Direction and Production: Anne G. Anderson This summer marks the 25th anniversary of the first flight of the Lockheed Hercules; a Volume 6, No. 3, July - September 1979 quarter century of service to nations throughout the world! Over 1,550 Hercules (C-130s Vol. 6, No. 3, July. September 1979 and L-100) have been delivered to 44 countries. We at Lockheed are very proud of this Contents: record and the reputation the Hercules has earned. It is a reputation built on depend- ability, versatility, and durability. 2 Focal Point The Hercules is a true workhorse. Many developing countries depend on it to carry all types of cargo, from lifesaving food to road-building equipment. They carry these cargoes to remote areas that are not easily accessible by any other mode of transporta- 3 tion. An additional advantage is its ability to land and take off in incredibly short 3 Crew Door Rigging distances, even on unpaved clearings. The tasks the Hercules is capable of accomplishing are almost limitless; from hunting hurricanes, to flying mercy relief missions. It is the universal airborne platform. And it is 14 Royal Norwegian Air Force energy-efficient, using only about half the fuel a comparable jet aircraft would require. 15 One of the more interesting aspects of these 25 years is that while the external design of 15 Hydraulic Pressure Drop the aircraft has changed very little, constant improvements in systems and avionics equip- ment have made the world’s outstanding cargo airplane also among the world’s most modern.
  • Suborbital Reusable Launch Vehicles and Applicable Markets

    Suborbital Reusable Launch Vehicles and Applicable Markets

    SUBORBITAL REUSABLE LAUNCH VEHICLES AND APPLICABLE MARKETS Prepared by J. C. MARTIN and G. W. LAW Space Launch Support Division Space Launch Operations October 2002 Space Systems Group THE AEROSPACE CORPORATION El Segundo, CA 90245-4691 Prepared for U. S. DEPARTMENT OF COMMERCE OFFICE OF SPACE COMMERCIALIZATION Herbert C. Hoover Building 14th and Constitution Ave., NW Washington, DC 20230 (202) 482-6125, 482-5913 Contract No. SB1359-01-Z-0020 PUBLIC RELEASE IS AUTHORIZED Preface This report has been prepared by The Aerospace Corporation for the Department of Commerce, Office of Space Commercialization, under contract #SB1359-01-Z-0020. The objective of this report is to characterize suborbital reusable launch vehicle (RLV) concepts currently in development, and define the military, civil, and commercial missions and markets that could capitalize on their capabilities. The structure of the report includes a brief background on orbital vs. suborbital trajectories, as well as an overview of expendable and reusable launch vehicles. Current and emerging market opportunities for suborbital RLVs are identified and discussed. Finally, the report presents the technical aspects and program characteristics of selected U.S. and international suborbital RLVs in development. The appendix at the end of this report provides further detail on each of the suborbital vehicles, as well as the management biographies for each of the companies. The integration of suborbital RLVs with existing airports and/or spaceports, though an important factor that needs to be evaluated, was not the focus of this effort. However, it should be noted that the RLV concepts discussed in this report are being designed to minimize unique facility requirements.
  • NATEP Innovation Directory Foreword

    NATEP Innovation Directory Foreword

    NATEP Innovation Directory Foreword Welcome to this directory of over 140 exciting R&T projects supported by NATEP, the National Aerospace Technology Exploitation Programme. NATEP assists companies in the aerospace supply chain to work collaboratively in the development of innovative technologies through a unique combination of match funding, mentoring and end user support. The mentoring is provided by a high calibre technical and management resource to help companies accelerate their technology development towards market readiness. Participation in the programme equips project partners to win new business with existing customers and to diversify their customer base. Since 2013 the programme has brought together National Aerospace Technology Exploitation Programme technology collaborations of more than 350 aerospace supply chain micro, small and medium sized companies. Funding new technologies and new manufacturing The technologies developed within the NATEP Programme will be used on productivity in the aerospace supply chain current and new aircraft programmes, increasing productivity, creating jobs and injecting new R&D capabilities into the supply chain. NATEP companies are supported to be better able to win work with existing customers and new customers, particularly in export markets, as well as in cross sectors markets such as the automotive, energy or rail sectors. The NATEP programme, is an Aerospace Growth Partnership initiative, dedicated to supporting the future of the aerospace sector in the UK. I hope that you will be interested
  • AOE 3104 Problem Sheet 10 (Ans) Our Class Business Jet Has the Following Characteristics

    AOE 3104 Problem Sheet 10 (Ans) Our Class Business Jet Has the Following Characteristics

    AOE 3104 Problem Sheet 10 (ans) Our class business jet has the following characteristics: Gross Weight = 10,000 lbs b = 40 ft CLmax = 1.8 (normal flight) 2 2 S = 200 ft CD = 0.02 + 0.05 (CL) CLmax = 2.4 (with flaps) 2 engines with 1000 lb / engine (up and away drag polar) During ground roll, the wing is 5 ft above the ground The coefficient of friction on the paved runway is : = 0.02 : The coefficient during braking is b = 0.3 51. Calculate the takeoff ground roll distance assuming no flaps are used for takeoff and that minimum takeoff distance conditions are used during the ground roll. Must calculate the conditions on the ground: However, units must be SI units so: and Then and The ground effect on the induced drag parameter K. Then the correction factor N is given by and Therefore This is the ground drag polar! For minimum distance takeoff, the proper ground lift coefficient is given by: The corresponding drag coefficient is determined from the ground drag polar” We can now calculate the constants in the takeoff equations: We need to calculate the reference speeds: Finally the takeoff distance can be calculated from: 52. Calculate the landing ground roll distance for this aircraft assuming a full flap landing and that zero lift occurs during the ground roll, and that brakes are applied at touch-down (short field landing in which you retract the flaps and hit the brakes as soon as possible after touch-down). Here we will assume that we land with flaps so we need to calculate new reference airspeeds: Ground run, no flaps.
  • Acquisition Story 54 Introduction 2 Who We Were 4 194Os 8 195Os 12

    Acquisition Story 54 Introduction 2 Who We Were 4 194Os 8 195Os 12

    table of contents Introduction 2 Who We Were 4 194Os 8 195Os 12 196Os 18 197Os 26 198Os 30 199Os 34 2OOOs 38 2O1Os 42 Historical Timeline 46 Acquisition Story 54 Who We Are Now 58 Where We Are Going 64 Vision For The Future 68 1 For nearly a century, innovation and reliability have been the hallmarks of two giant U.S. aerospace icons – Aerojet and Rocketdyne. The companies’ propulsion systems have helped to strengthen national defense, launch astronauts into space, and propel unmanned spacecraft to explore the universe. ➢ Aerojet’s diverse rocket propulsion systems have powered military vehicles for decades – from rocket-assisted takeoff for propeller airplanes during World War II – through today’s powerful intercontinental ballistic missiles (ICBMs). The systems helped land men on the moon, and maneuvered spacecraft beyond our solar system. ➢ For years, Rocketdyne engines have played a major role in national defense, beginning with powering the United States’ first ICBM to sending modern military communication satellites into orbit. Rocketdyne’s technology also helped launch manned moon missions, propelled space shuttles, and provided the main power system for the International Space Station (ISS). ➢ In 2013, these two rocket propulsion manufacturers became Aerojet Rocketydne, blending expertise and vision to increase efficiency, lower costs, and better compete in the market. Now, as an industry titan, Aerojet Rocketdyne’s talented, passionate employees collaborate to create even greater innovations that protect America and launch its celestial future. 2011 A Standard Missile-3 (SM-3) interceptor is being developed as part of the U.S. Missile Defense Agency’s sea-based Aegis Ballistic Missile Defense System.
  • THE YEAR in REVIEW a PUBLICATION of the AMERICAN INSTITUTE of AERONAUTICS and ASTRONAUTICS Toc-December.Qxd:AA Template 11/19/10 11:42 AM Page 1

    THE YEAR in REVIEW a PUBLICATION of the AMERICAN INSTITUTE of AERONAUTICS and ASTRONAUTICS Toc-December.Qxd:AA Template 11/19/10 11:42 AM Page 1

    FC_Aerospace_DEC2010_pms.pdf 11/22/10 10:33:41 AM coverƒ-1210.qxd:AA Template 11/17/10 9:53 AM Page 1 11 AMERICA AEROSPACE December 2010 DECEMBER 2010 C M Y CM MY CY CMY K 2010THE YEAR IN REVIEW A PUBLICATION OF THE AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS toc-December.qxd:AA Template 11/19/10 11:42 AM Page 1 December 2010 EDITORIAL 3 OUT OF THE PAST 76 2010 SUBJECT AND AUTHOR INDEX 78 CAREER OPPORTUNITIES 84 THE YEAR IN REVIEW Adaptive structures 5 Intelligent systems 41 Aeroacoustics 19 Life sciences 58 Aerodynamic decelerators 30 Lighter-than-air systems 26 Aerodynamic measurement Liquid propulsion 55 technology 17 Management 38 Aerospace power systems 54 Materials 8 Aerospace traffic management 73 Meshing, visualization and Air-breathing propulsion systems computational environments 6 integration 56 Missile systems 61 Aircraft design 32 Modeling and simulation 24 Aircraft operations 33 Multidisciplinary design Applied aerodynamics 21 optimization 12 Astrodynamics 18 Nondeterministic approaches 10 Atmospheric and space Nuclear and future flight environments 23 propulsion 52 Atmospheric flight mechanics 22 Plasmadynamics and lasers 14 Balloon systems 28 Propellants and combustion 50 Communication systems 43 Sensor systems 45 Computer-aided enterprise Society and aerospace technology 36 solutions 35 Software systems 40 Computer systems 42 Solid rockets 47 Design engineering 4 Space colonization 64 Digital avionics 44 Space exploration 71 Directed energy systems 74 Space logistics 63 Economics 37 Space operations and support