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Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber. -
Analysis of Aircraft for the Fire Fighting Mission in Colorado
Analysis of the Alenia C-27J, British Aerospace 146-200, Lockheed S-3B and Lockheed C-130H/Q Aircraft for the Fire Fighting Mission in Colorado. December 6, 2013 Prepared by: Conklin & de Decker Aviation Information Arlington, TX 76012 817 277 6403 www.conklindd.com Analysis of C-27J, BAe 146, S-3B and C-130H/Q for the Fire Fighting Mission in Colorado Conklin & de Decker Aviation Information, December 6, 2013 Table of Contents Page 1 Summary and Conclusions.......................................................................................... 3 2 Introduction ................................................................................................................ 5 3 Aircraft Analyzed......................................................................................................... 6 3.1 Alenia C-27J......................................................................................................... 6 3.1.1 Retardant Tank Capacity............................................................................. 7 3.2 British Aerospace BAe-146 ................................................................................. 9 3.2.1 Retardant Tank Capacity........................................................................... 10 3.3 Lockheed C-130H/Q.......................................................................................... 11 3.3.1 Retardant Tank Capacity........................................................................... 12 3.4 Lockheed S-3B.................................................................................................. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2015. By Aaron M. U. Church, Senior Editor ■ 2016 USAF Almanac BOMBER AIRCRAFT B-1 Lancer Brief: Long-range bomber capable of penetrating enemy defenses and de- livering the largest weapon load of any aircraft in the inventory. COMMENTARY The B-1A was initially proposed as replacement for the B-52, and four proto- types were developed and tested before program cancellation in 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft added 74,000 lb of usable payload, improved radar, and reduced radar cross section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in Iraq during Desert Fox in December 1998. Its three internal weapons bays accommodate a substantial payload of weapons, including a mix of different weapons in each bay. Lancer production totaled 100 aircraft. The bomber’s blended wing/ body configuration, variable-geometry design, and turbofan engines provide long range and loiter time. The B-1B has been upgraded with GPS, smart weapons, and mission systems. Offensive avionics include SAR for tracking, B-2A Spirit (SSgt. Jeremy M. Wilson) targeting, and engaging moving vehicles and terrain following. GPS-aided INS lets aircrews autonomously navigate without ground-based navigation aids Dimensions: Span 137 ft (spread forward) to 79 ft (swept aft), length 146 and precisely engage targets. Sniper pod was added in 2008. The ongoing ft, height 34 ft. integrated battle station modifications is the most comprehensive refresh in Weight: Max T-O 477,000 lb. -
Etu – V Tulpar
2017-2018 Undergraduate Team Engine Candidate Engines for a Next Generation Supersonic Transport ETU – V TULPAR TEAM MEMBERS Veli Can ÜSTÜNDAĞ - 921399 Çağdaş Cem ERGİN - 920976 Baran İPER - 921398 Onur TAN - 921395 Faculty Advisor Asst. Prof. Sıtkı USLU SIGNATURES Faculty Advisor Asst. Prof. Sıtkı USLU TOBB University of Economics and Technology Team Leader Cagdas Cem ERGIN TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 920976 Team Member Veli Can USTUNDAG TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 921399 Team Member Baran IPER TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 921398 Team Member Onur TAN TOBB University of Economics and Technology Deparment of Mechanical Engineering AIAA Member Number: 921395 ii TABLE OF CONTENT LIST OF TABLES .................................................................................................................................................. v LIST OF FIGURES ............................................................................................................................................... vi NOMENCLATURE ............................................................................................................................................... ix 1. INTRODUCTION .......................................................................................................................................... 1 2. STATE OF THE -
Usafalmanac ■ Gallery of USAF Weapons
USAFAlmanac ■ Gallery of USAF Weapons By Susan H.H. Young fans; each 17,300 lb thrust. Accommodation: two, mission commander and pilot, Bombers on zero/zero ejection seats. B-1 Lancer Dimensions: span 172 ft, length 69 ft, height 17 ft. Brief: A long-range multirole bomber capable of flying Weight: empty 150,000–160,000 lb, gross 350,000 lb. missions over intercontinental range without refueling, then Performance: minimum approach speed 161 mph, penetrating enemy defenses with a heavy load of ordnance. ceiling 50,000 ft, typical estimated unrefueled range for a Function: Long-range conventional bomber. hi-lo-hi mission with 16 B61 nuclear free-fall bombs 5,000 Operator: ACC, ANG. miles, with one aerial refueling more than 10,000 miles. First Flight: Dec. 23, 1974 (B-1A); October 1984 (B-1B). Armament: in a nuclear role: up to 16 nuclear weapons Delivered: June 1985–May 1988. (B-61, B-61 Mod II, B-83). In a conventional role: 16 Mk 84 2,000-lb bombs, up to 16 2,000-lb GBU-36/B (GAM), or up IOC: Oct. 1, 1986, Dyess AFB, Texas (B-1B). B-1B Lancer (Ted Carlson) Production: 104. to eight 4,700-lb GBU-37 (GAM-113) near–precision guided Inventory: 94 (B-1B). weapons. Various other conventional weapons, incl the Mk Ceiling: over 30,000 ft. Unit Location: Active: Dyess AFB, Texas, Ellsworth AFB, S.D., and Mountain Home AFB, Idaho. ANG: McConnell AFB, Kan., and Robins AFB, Ga. Contractor: Boeing North American; AIL Systems; General Electric. Power Plant: four General Electric F101-GE-102 turbo- fans; each 30,780 lb thrust. -
Development of Dynamic Simulation of TF34-GE-100 Turbofan Engine with Post-Stall Capability
-- NASA Technical Memorandum 83660 AIAA-84-1184 NASA-TM-83660 /_o°4oo/'76q4/ Development of Dynamic Simulation of TF34-GE-100 Turbofan Engine with Post-Stall Capability Susan M. Krosel Lewis Research Center Cleveland, Ohio a i : t ii l__,12L.--'.'i. ' - _.227'.T-2 L'. :..,2 ' " ' H:, . ,.. .... A Prepared for the Twentieth Joint Propulsion Conference cosponsored by the AIAA, SAE, and ASME Cincinnati, Ohio, June 11-13, 1984 1 RN/NASA-TM-S3SGG ~-21G4 NAS 1.15~S366e AiHA-24-1184 11 PAGES t !TT~ '; -+ i ,.:,::!-...-.:.:! -, ..-.. •...: 1 1 L: \.'-:, ""'"••...., I Cl I Natio~cil A2fO~dUt!CS Clev~idnd, Ohio. --'- +~-_r-... cit \.;;-= 11-13 .Jurl. MAJS~ /*ANALOG COMPUTERS/*COMPUTERIZED SIMULATION/*ENGINE FAILURE/*TURSOFAN DIGITAL CQMPUTERS/ MATHEMAT1CAL MODELS; PERFORMANCE TESTS/ REAL OPERAT i f}f-J -----------------------------------------_.....----------~~ AIAA-84-1184 Developmentof DynamicSimulationof TF34-GE-100TurbofanEnginewith Post-StallCapability SusanM. Krosel,NASALewisResearch Center,Cleveland,OH AIAA/SAE/ASIVlE 20thJointPropulsionConference June 11-13,1984/Cincinnati,Ohio Forpermissiontocopyorrepublishcontact, theAmericanInstituteofAeronauticsandAstronautics 1633Broadway,NewYork,NY10019 DEVELOPMENTOF DYNAMICSIMULATIONOF TF34-GE-100TURBOFAN ENGINEWITH POST-STALLCAPABILITY SusanM. Krosel NationalAeronauticsand SpaceAdministration LewisResearchCenter Cleveland,Ohio 44135 Abstract TB turbine f fuel This paper describes the development of a i initial condition hybrid computer simulation of a TF34-GE-IO0 turbo- in into volume fan engine with post-stall capability. The simu- out out of volume lation operates in real-time and will be used to test and evaluate stall recovery control modes for Introduction this engine. The simulation calculations are per- formed by an analog computer with a peripheral The desire for increased performance from multivariable function generation unit used for aircraft gas turbine engines has resulted in computing bivariate functions. -
Modern Combat Aircraft (1945 – 2010)
I MODERN COMBAT AIRCRAFT (1945 – 2010) Modern Combat Aircraft (1945-2010) is a brief overview of the most famous military aircraft developed by the end of World War II until now. Fixed-wing airplanes and helicopters are presented by the role fulfilled, by the nation of origin (manufacturer), and year of first flight. For each aircraft is available a photo, a brief introduction, and information about its development, design and operational life. The work is made using English Wikipedia, but also other Web sites. FIGHTER-MULTIROLE UNITED STATES UNITED STATES No. Aircraft 1° fly Pg. No. Aircraft 1° fly Pg. Lockheed General Dynamics 001 1944 3 011 1964 27 P-80 Shooting Star F-111 Aardvark Republic Grumman 002 1946 5 012 1970 29 F-84 Thunderjet F-14 Tomcat North American Northrop 003 1947 7 013 1972 33 F-86 Sabre F-5E/F Tiger II North American McDonnell Douglas 004 1953 9 014 1972 35 F-100 Super Sabre F-15 Eagle Convair General Dynamics 005 1953 11 015 1974 39 F-102 Delta Dagger F-16 Fighting Falcon Lockheed McDonnell Douglas 006 1954 13 016 1978 43 F-104 Starfighter F/A-18 Hornet Republic Boeing 007 1955 17 017 1995 45 F-105 Thunderchief F/A-18E/F Super Hornet Vought Lockheed Martin 008 1955 19 018 1997 47 F-8 Crusader F-22 Raptor Convair Lockheed Martin 009 1956 21 019 2006 51 F-106 Delta Dart F-35 Lightning II McDonnell Douglas 010 1958 23 F-4 Phantom II SOVIET UNION SOVIET UNION No. -
National Air & Space Museum Technical Reference Files: Propulsion
National Air & Space Museum Technical Reference Files: Propulsion NASM Staff 2017 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Scope and Contents........................................................................................................ 1 Accessories...................................................................................................................... 1 Engines............................................................................................................................ 1 Propellers ........................................................................................................................ 2 Space Propulsion ............................................................................................................ 2 Container Listing ............................................................................................................. 3 Series B3: Propulsion: Accessories, by Manufacturer............................................. 3 Series B4: Propulsion: Accessories, General........................................................ 47 Series B: Propulsion: Engines, by Manufacturer.................................................... 71 Series B2: Propulsion: Engines, General............................................................ -
Gallery of USAF Weapons
Almanac USAF■ Gallery of USAF Weapons By Susan H.H. Young Note: Inventory numbers are Total Active Inventory figures as of Sept. 30, 1999. B-1B’s list of weapons, with fleet completion in FY02. The B-1B’s capability is being significantly enhanced by the ongoing Conventional Mission Upgrade Pro- gram (CMUP). This gives the B-1B greater lethality and survivability through the integration of precision and standoff weapons and a robust ECM suite. CMUP includes GPS receivers, a MIL-STD-1760 weapon in- terface, secure radios, and improved computers to support precision weapons, initially the JDAM, fol- lowed by the Joint Standoff Weapon (JSOW) and the Joint Air-to-Surface Standoff Missile (JASSM). The Defensive System Upgrade Program will improve air- crew situational awareness and jamming capability. B-2 Spirit Brief: Stealthy, long-range, multirole bomber that can deliver conventional and nuclear munitions any- where on the globe by flying through previously impen- etrable defenses. Function: Long-range heavy bomber. Operator: ACC. First Flight: July 17, 1989. Delivered: Dec. 17, 1993–present. B-1B Lancer (Ted Carlson) IOC: April 1997, Whiteman AFB, Mo. Production: 21. Inventory: 21. Unit Location: Whiteman AFB, Mo. Contractor: Northrop Grumman, with Boeing, LTV, and General Electric as principal subcontractors. Bombers Power Plant: four General Electric F118-GE-100 turbofans, each 17,300 lb thrust. B-1 Lancer Accommodation: two, mission commander and pi- Brief: A long-range multirole bomber capable of lot, on zero/zero ejection seats. flying missions over intercontinental range without re- Dimensions: span 172 ft, length 69 ft, height 17 ft. -
An Analysis of Single-Engine Rate-Of-Climb Capabilities and Thrust
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1995-06 An analysis of single-engine rate-of-climb capabilities and thrust requirements of the S-3 and ES-3 aircraft in support of the TF34 Engine Component Improvement Program Micklewright, Alan J. Monterey, California. Naval Postgraduate School http://hdl.handle.net/10945/31468 NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA THESIS AN ANALYSIS OF SINGLE-ENGINE RATE-OF-CLIMB CAPABILITIES AND THRUST REQUIREMENTS OF THE S-3 AND ES-3 AHtCRAFT IN SUPPORT OF THE TF34 ENGINE COMPONENT IMPROVEMENT PROGRAM by Alan J. Micklewright June 1995 Principal Advisor: Donald R. Eaton Antirnvd f "blic release; distribution is unlimited. 19960116 035 DEKJ QOäA*d\n :.x;-rßß l. REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington DC 20503. AGENCY USE ONLY (Leave blank) REPORT DATE 3. REPORT TYPE AND DATES COVERED June 1995 Master's Thesis 4. TITLE AND SUBTITLE AN ANALYSIS OF SINGLE-ENGINE RATE- FUNDING NUMBERS OF-CLIMB CAPABILITIES AND THRUST REQUIREMENTS OF THE S-3 AND ES-3 AIRCRAFT IN SUPPORT OF THE TF34 ENGINE COMPONENT IMPROVEMENT PROGRAM. -
2013 USAF Almanac
May 2013/$8 May 2013 USAF Almanac AIR FORCE MAGAZINE MAY 2013 ALMANAC WWW.AIRFORCEMAG.COM Sensing Effects C4I Training & Logistics Cyber MISSION: MODERNIZE WITHOUT COMPROMISE Raytheon’s drop-in, plug-and-play technology is turning older aircraft into cutting-edge fi ghters, allowing countries to maximize their fl eets even in a time of tighter budgets. By enhancing pilot awareness and empowering platforms, we’re enabling tomorrow’s missions, today. See how RACR is bringing plug-and-play, state-of-the-art performance to today’s fi ghter jets at: Raytheon.com © 2013 Raytheon Company. All rights reserved. “Customer Success Is Our Mission” is a registered trademark of Raytheon Company. 13SAS243_MISSIONModern_AFAlam_May2013.indd 1 3/21/13 11:40 AM Sensing Effects C4I Training & Logistics Cyber MISSION: MODERNIZE WITHOUT COMPROMISE Raytheon’s drop-in, plug-and-play technology is turning older aircraft into cutting-edge fi ghters, allowing countries to maximize their fl eets even in a time of tighter budgets. By enhancing pilot awareness and empowering platforms, we’re enabling tomorrow’s missions, today. See how RACR is bringing plug-and-play, state-of-the-art performance to today’s fi ghter jets at: Raytheon.com © 2013 Raytheon Company. All rights reserved. “Customer Success Is Our Mission” is a registered trademark of Raytheon Company. 13SAS243_MISSIONModern_AFAlam_May2013.indd 1 3/21/13 11:40 AM 2013 USAF Almanac May 2013, Vol. 96, No. 5 May 2013, Vol. 96, No. 5 6 Editorial: How to Lose a Sprint and a Marathon Publisher By Adam J. Hebert Craig R. McKinley Under sequestration, readiness is no longer assured.