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RH-53D Sea Stallion - 1984, 30X
RH-53D Sea Stallion - 1984, 30x United States Type: Mine Sweeper (MCM) Min Speed: 30 kt Max Speed: 155 kt Commissioned: 1984 Length: 22.3 m Wingspan: 9.0 m Height: 7.6 m Crew: 5 Empty Weight: 10740 kg Max Weight: 19100 kg Max Payload: 8000 kg Propulsion: 3x T64-GE-413A Sensors / EW: - AN/APR-39(V)2 - (USN/USMC) ESM, RWR, Radar Warning Receiver, Max range: 222.2 km - Generic Navigation Radar - (USN/USMC) Radar, Radar, Navigation, Max range: 37 km - Generic FLIR - (2nd Gen, Surveillance, 8x Magnification) Infrared, Infrared, Surveillance Camera, Max range: 55.6 km Weapons / Loadouts: - Mk103 Helicopter-Towed Mechanical Cable Cutter Mine Sweep - Helicopter-Towed Package. - Mk104 Helicopter-Towed Acoustic Influence Mine Sweep - Helicopter-Towed Package. - Mk105 Helicopter-Towed Magnetic Influence Mine Sweep - Helicopter-Towed Package. - Mk106 [Mk104 & Mk105] Helicopter-Towed Magnetic & Acoustic Multi-Influence Mine Sweep - (1971) Helicopter-Towed Package. - AN/AQS-14 Helicopter-Towed Minehunting Sonar - (1985) Helicopter-Towed Package. OVERVIEW: The CH-53 Sea Stallion is the most common name for the Sikorsky S-65 family of heavy-lift transport helicopters. Originally developed for use by the United States Marine Corps, it is also in service with Germany, Iran, Israel, and Mexico. The United States Air Force operated the HH-53 "Super Jolly Green Giant" during the late- and post-Vietnam War era, updating most of them as the MH-53 Pave Low. The dimensionally-similar CH-53E Super Stallion is a heavier-lifting, improved version designated S-80E by Sikorsky. Its third engine makes it more powerful than the Sea Stallion, which it has replaced in the heavy-lift mission. -
2018 Annual Report Our Leadership Team (From Left to Right): Frank A
FINANCIAL HIGHLIGHTS In millions, except per share data 2018 2017 2016 Net Sales $53,762 $49,960 $47,290 Segment Operating Profit 5,877 5,092 4,982 Consolidated Operating Profit 7,334 6,744 5,888 Net Earnings From Continuing Operations 5,046 1,890 3,661 Net Earnings 5,046 1,963 5,173 Diluted Earnings Per Common Share Continuing Operations 17.59 6.50 12.08 Net Earnings 17.59 6.75 17.07 Cash Dividends Per Common Share 8.20 7.46 6.77 Average Diluted Common Shares Outstanding 287 291 303 Cash and Cash Equivalents $772$ 2,861 $ 1,837 Total Assets 44,876 46,620 47,560 Total Debt, net 14,104 14,263 14,282 Total Equity (Deficit) 1,449 (776) 1,477 Common Shares Outstanding at Year-End 281 284 289 Net Cash Provided by Operating Activities $3,138 $ 6,476 $ 5,189 NOTE: For additional information regarding the amounts presented above, see the Form 10-K portion of this Annual Report. A reconciliation of Segment Operating Profit to Consolidated Operating Profit is included on the page preceding the back cover of this Annual Report. On the Cover: F-35B Lightning II On September 29, 2018, the first F-35B Lightning II stealth fighters landed on the flight deck of HMS Queen Elizabeth, as Britain’s newest Royal Navy aircraft carrier conducted trials off the Eastern Seaboard of the United States. These developmental trials included more than 500 take-offs and landings from the warship over an 11-week period. The F-35B is one of three variants of the world’s most advanced supersonic fifth-generation fighter jet. -
Electronic Warfare Fundamentals
ELECTRONIC WARFARE FUNDAMENTALS NOVEMBER 2000 PREFACE Electronic Warfare Fundamentals is a student supplementary text and reference book that provides the foundation for understanding the basic concepts underlying electronic warfare (EW). This text uses a practical building-block approach to facilitate student comprehension of the essential subject matter associated with the combat applications of EW. Since radar and infrared (IR) weapons systems present the greatest threat to air operations on today's battlefield, this text emphasizes radar and IR theory and countermeasures. Although command and control (C2) systems play a vital role in modern warfare, these systems are not a direct threat to the aircrew and hence are not discussed in this book. This text does address the specific types of radar systems most likely to be associated with a modern integrated air defense system (lADS). To introduce the reader to EW, Electronic Warfare Fundamentals begins with a brief history of radar, an overview of radar capabilities, and a brief introduction to the threat systems associated with a typical lADS. The two subsequent chapters introduce the theory and characteristics of radio frequency (RF) energy as it relates to radar operations. These are followed by radar signal characteristics, radar system components, and radar target discrimination capabilities. The book continues with a discussion of antenna types and scans, target tracking, and missile guidance techniques. The next step in the building-block approach is a detailed description of countermeasures designed to defeat radar systems. The text presents the theory and employment considerations for both noise and deception jamming techniques and their impact on radar systems. -
Loran C Cycle Matching Operational Evaluation in North Pacific Area
~Opy 19 Report No. FAA ...RD-75-142 1-= FAA WJH Technical Center 1111\\\ 11\\1 11m 11111 11m 11111 1III1 11111 11111111 00090609 LORAN C CYCLE MATCHING OPERATIONAL EVALUATION IN NORTH PACIFIC AREA Jon R. Hamilton . .. NAFEC :~. LIBRARY DEC 2197~· # . October 1975 Final Report Document is avai lable to the public through the National Technical Information Service, Springfield, Virginia 22161. Preparell for u.s. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION Systems Research &Development Service Washington, D.C. 20590 NOTICE This document is disseminated under the sponsorship of the Department of Transportation in the interest of infor mation exchange. The United States Government assumes no liability for its contents or use thereof. 1 -=~,....e;.,...~_r~_~.,...~.,...' ~T 'I";~T,iW', 1--:-_' -..,..7_5..,..-_1_4_2 ....'·-O:;;;;-"=;;;;=:--.-- (000'0' No 4. Tit'e and Subtitle 5. Rer,ort Dote Loran C Cycle Matching Operational Evaluation in October 1975 North Pacific Area I-:- ------::-------:::----~--_1 1'-::--:---:--:-:---------------------------- ,g. P .. rio-Ming Orgonlzation Report N.o. 7. Author/ .) Jon R. Hami 1ton P~rfo,mi"g 9. l.Ontlnenta Organitotjpi) I-\lr N.p[e. lneS, and Acld'fu nco In. Wark Unit No. /TRAIS) International Airport 11. Cont'oct or Grant No. Los Angeles, California 90009 DOT -FA75WA-3607 -:-. '--'~"--"----'-'" ._.--------- 1J. 1" yp.. "f Qepc"t 01"1' Period Coy"r.d ~-....,.....-----_._---_._._._----.-_._--.-. __._._.__..._. __ ._---._.._." 12. Sponsoring Agency Name and ~cldr..". Final Department of Transportation I October 1975 Federal Aviation Administration Systems Research and Development Service 14. Spc.nsorinll Agene./ Code Washington, D. -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
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, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998. -
(12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz Et Al
USOO88695 04B1 (12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz et al. (45) Date of Patent: Oct. 28, 2014 (54) GEAREDTURBOFAN ENGINE GEARBOX 5.431,539 A 7/1995 Carvalho ARRANGEMENT 5,443,365 A * 8/1995 Ingling et al. ............. 416, 193A 5,778,659 A 7/1998 Duesler et al. 6,464,401 B1 10/2002 Allard (71) Applicant: United Technologies Corporation, 7,144.221 B2 * 12/2006 Giffin ............................ 416,189 Hartford, CT (US) 8,137,070 B2 * 3/2012 Van Houten ... 416,189 2006.0024162 A1* 2, 2006 Giffin .......... ... 415,208.3 (72) Inventors: Frederick M. Schwarz, Glastonbury, 2007/015.1258 A1* 7/2007 Gaines et al. ................... 60,792 CT (US); William G. Sheridan, 2008/00987.17 A1* 5, 2008 Orlando et al. .... ... 60,226.1 Southington, CT (US) 2010/0218478 A1* 9/2010 Merry et al. .................... 60,205 glon, 2011/0056208 A1 3/2011 Norris et al. .................... 6Of772 2011/O123326 A1 5/2011 DiBenedetto et al. (73) Assignee: United Technologies Corporation, 2012/0110979 A1* 5, 2012 Rosenkrans et al. ......... 60,226.1 Hartford, CT (US) 2012fO251306 A1* 10/2012 Reinhardt et al. ......... 415, 1821 2012fO263579 A1* 10, 2012 Otto et al. .......... ... 415,124.2 (*) Notice: Subject to any disclaimer, the term of this 2012/0291449 A1* 11/2012 Adams et al. ................... 60,793 2012/03 15130 A1 12/2012 Hasel et al. patent is extended or adjusted under 35 2013, OO25257 A1 1/2013 Suciu et all U.S.C. 154(b) by 0 days. 2013/0025258 A1* 1/2013 Merry et al. -
Technical Report
NAVAL POSTGRADUATE SCHOOL Monterey, California TECHNICAL REPORT “SEA ARCHER” Distributed Aviation Platform by Faculty Members Charles Calvano David Byers Robert Harney Fotis Papoulias John Ciezki Robert Ashton Student Members LT Joe Keller, USN LCDR Rabon Cooke, USN CDR(sel) James Ivey, USN LT Brad Stallings, USN LT Antonios Dalakos, Helenic Navy LT Scot Searles, USN LTjg Orhan Okan, Turkish Navy LTjg Mersin Gokce, Turkish Navy LT Ryan Kuchler, USN LT Pete Lashomb, USN Ivan Ng, Singapore December 2001 Approved for public release, distribution unlimited 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. 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED December 2001 Technical Report 4. TITLE AND SUBTITLE: 5. FUNDING NUMBERS “Sea Archer” Distributed Aviation Platform 6. AUTHOR(S) Charles Calvano, Robert Harney, David Byers, Fotis Papoulias, John Ciezki, LT Joe Keller, LCDR Rabon Cooke, CDR (sel) James Ivey, LT Brad Stallings, LT Scot Searles, LT Ryan Kuchler, Ivan Ng, LTjg Orhan Okan, LTjg Mersin Gokce, LT Antonios Dalakos, LT Pete Lashomb. -
Federal Register/Vol. 85, No. 239/Friday, December 11, 2020
80060 Federal Register / Vol. 85, No. 239 / Friday, December 11, 2020 / Notices Defense System Launcher political stability, military balance, 2. The highest level of classification of Transporter Units, twenty-five (25) economic and progress in the region. defense articles, components, and radar trucks, spare and repair parts, This proposed sale will improve the services included in this potential sale support and test equipment, recipient’s capability to meet current is CONFIDENTIAL. publications and technical and future threats by providing a 3. If a technologically advanced documentation, personnel training flexible solution to augment existing adversary were to obtain knowledge of and training equipment, U.S. surface and air defenses. The recipient the hardware and software elements, the Government and contractor will be able to employ a highly reliable information could be used to develop representatives’ technical and effective system to counter or deter countermeasures or equivalent systems, assistance, engineering and logistics maritime aggressions, coastal blockades, which might reduce system support services, and other related and amphibious assaults. This effectiveness or be used in the elements of logistics support. capability will easily integrate into development of a system with similar or (iv) Military Department: Navy (TW-P- existing force infrastructure. The advanced capabilities. LHX) recipient will have no difficulty 4. A determination has been made (v) Prior Related Cases, if any: TW-P- absorbing these systems into its armed that the recipient can provide LGV, TW-P-LGN, TW-P-LGL forces. substantially the same degree of (vi) Sales Commission, Fee, etc., Paid, The proposed sale of this equipment protection for the sensitive technology Offered, or Agreed to be Paid: None and support will not alter the basic (vii) Sensitivity of Technology being released as the U.S. -
Chapter 2 HISTORY and DEVELOPMENT of MILITARY LASERS
History and Development of Military Lasers Chapter 2 HISTORY AND DEVELOPMENT OF MILITARY LASERS JACK B. KELLER, JR* INTRODUCTION INVENTING THE LASER MILITARIZING THE LASER SEARCHING FOR HIGH-ENERGY LASER WEAPONS SEARCHING FOR LOW-ENERGY LASER WEAPONS RETURNING TO HIGHER ENERGIES SUMMARY *Lieutenant Colonel, US Army (Retired); formerly, Foreign Science Information Officer, US Army Medical Research Detachment-Walter Reed Army Institute of Research, 7965 Dave Erwin Drive, Brooks City-Base, Texas 78235 25 Biomedical Implications of Military Laser Exposure INTRODUCTION This chapter will examine the history of the laser, Military advantage is greatest when details are con- from theory to demonstration, for its impact upon the US cealed from real or potential adversaries (eg, through military. In the field of military science, there was early classification). Classification can remain in place long recognition that lasers can be visually and cutaneously after a program is aborted, if warranted to conceal hazardous to military personnel—hazards documented technological details or pathways not obvious or easily in detail elsewhere in this volume—and that such hazards deduced but that may be relevant to future develop- must be mitigated to ensure military personnel safety ments. Thus, many details regarding developmental and mission success. At odds with this recognition was military laser systems cannot be made public; their the desire to harness the laser’s potential application to a descriptions here are necessarily vague. wide spectrum of military tasks. This chapter focuses on Once fielded, system details usually, but not always, the history and development of laser systems that, when become public. Laser systems identified here represent used, necessitate highly specialized biomedical research various evolutionary states of the art in laser technol- as described throughout this volume. -
Helicopter Turboshafts
Helicopter Turboshafts Luke Stuyvenberg University of Colorado at Boulder Department of Aerospace Engineering The application of gas turbine engines in helicopters is discussed. The work- ings of turboshafts and the history of their use in helicopters is briefly described. Ideal cycle analyses of the Boeing 502-14 and of the General Electric T64 turboshaft engine are performed. I. Introduction to Turboshafts Turboshafts are an adaptation of gas turbine technology in which the principle output is shaft power from the expansion of hot gas through the turbine, rather than thrust from the exhaust of these gases. They have found a wide variety of applications ranging from air compression to auxiliary power generation to racing boat propulsion and more. This paper, however, will focus primarily on the application of turboshaft technology to providing main power for helicopters, to achieve extended vertical flight. II. Relationship to Turbojets As a variation of the gas turbine, turboshafts are very similar to turbojets. The operating principle is identical: atmospheric gases are ingested at the inlet, compressed, mixed with fuel and combusted, then expanded through a turbine which powers the compressor. There are two key diferences which separate turboshafts from turbojets, however. Figure 1. Basic Turboshaft Operation Note the absence of a mechanical connection between the HPT and LPT. An ideal turboshaft extracts with the HPT only the power necessary to turn the compressor, and with the LPT all remaining power from the expansion process. 1 of 10 American Institute of Aeronautics and Astronautics A. Emphasis on Shaft Power Unlike turbojets, the primary purpose of which is to produce thrust from the expanded gases, turboshafts are intended to extract shaft horsepower (shp). -
Program Acquisition Cost by Weapon System Major Weapon Systems OVERVIEW
The estimated cost of this report or study for the Department of Defense is approximately $32,000 for the 2017 Fiscal Year. This includes $13,000 in expenses and $19,000 in DoD labor. Generated on 2017May03 RefID: E-7DE12B0 FY 2018 Program Acquisition Cost by Weapon System Major Weapon Systems OVERVIEW The combined capabilities and performance of United States (U.S.) weapon systems are unmatched throughout the world, ensuring that U.S. military forces have the advantage over any adversary. The Fiscal Year (FY) 2018 acquisition funding request for the Department of Defense (DoD) budget totals $208.6 billion, which includes base funding and Overseas Contingency Operations (OCO) funding; $125.2 billion for Procurement funded programs and $83.3 billion for Research, Development, Test, and Evaluation (RDT&E) funded programs. Of the $208.6 billion, $94.9 billion is for programs that have been designated as Major Defense Acquisition Programs (MDAPs). This book focuses on all funding for the key MDAP programs. To simplify the display of the various weapon systems, this book is organized by the following mission area categories: Mission Area Categories • Aircraft & Related Systems • Missiles and Munitions • Command, Control, Communications, • Mission Support Activities Computers, and Intelligence (C4I) Systems • RDT&E Science & Technology • Ground Systems • Shipbuilding and Maritime Systems • Missile Defense Programs • Space Based Systems FY 2018 Modernization – Total: $208.6 Billion ($ in Billions) Space Based Aircraft & Systems Related $9.8