Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept
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From the Line in the Sand: Accounts of USAF Company Grade Officers In
~~may-='11 From The Line In The Sand Accounts of USAF Company Grade Officers Support of 1 " 1 " edited by gi Squadron 1 fficer School Air University Press 4/ Alabama 6" March 1994 Library of Congress Cataloging-in-Publication Data From the line in the sand : accounts of USAF company grade officers in support of Desert Shield/Desert Storm / edited by Michael P. Vriesenga. p. cm. Includes index. 1. Persian Gulf War, 1991-Aerial operations, American . 2. Persian Gulf War, 1991- Personai narratives . 3. United States . Air Force-History-Persian Gulf War, 1991 . I. Vriesenga, Michael P., 1957- DS79 .724.U6F735 1994 94-1322 959.7044'248-dc20 CIP ISBN 1-58566-012-4 First Printing March 1994 Second Printing September 1999 Third Printing March 2001 Disclaimer This publication was produced in the Department of Defense school environment in the interest of academic freedom and the advancement of national defense-related concepts . The views expressed in this publication are those of the authors and do not reflect the official policy or position of the Department of Defense or the United States government. This publication hasbeen reviewed by security andpolicy review authorities and is clearedforpublic release. For Sale by the Superintendent of Documents US Government Printing Office Washington, D.C . 20402 ii 9&1 gook L ar-dicat£a to com#an9 9zacL orflcF-T 1, #ait, /2ZE4Ent, and, E9.#ECLaL6, TatUlLE. -ZEa¢ra anJ9~ 0 .( THIS PAGE INTENTIONALLY LEFT BLANK Contents Essay Page DISCLAIMER .... ... ... .... .... .. ii FOREWORD ...... ..... .. .... .. xi ABOUT THE EDITOR . ..... .. .... xiii ACKNOWLEDGMENTS . ..... .. .... xv INTRODUCTION .... ..... .. .. ... xvii SUPPORT OFFICERS 1 Madzuma, Michael D., and Buoniconti, Michael A. -
Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
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. -
Comparison of Helicopter Turboshaft Engines
Comparison of Helicopter Turboshaft Engines John Schenderlein1, and Tyler Clayton2 University of Colorado, Boulder, CO, 80304 Although they garnish less attention than their flashy jet cousins, turboshaft engines hold a specialized niche in the aviation industry. Built to be compact, efficient, and powerful, turboshafts have made modern helicopters and the feats they accomplish possible. First implemented in the 1950s, turboshaft geometry has gone largely unchanged, but advances in materials and axial flow technology have continued to drive higher power and efficiency from today's turboshafts. Similarly to the turbojet and fan industry, there are only a handful of big players in the market. The usual suspects - Pratt & Whitney, General Electric, and Rolls-Royce - have taken over most of the industry, but lesser known companies like Lycoming and Turbomeca still hold a footing in the Turboshaft world. Nomenclature shp = Shaft Horsepower SFC = Specific Fuel Consumption FPT = Free Power Turbine HPT = High Power Turbine Introduction & Background Turboshaft engines are very similar to a turboprop engine; in fact many turboshaft engines were created by modifying existing turboprop engines to fit the needs of the rotorcraft they propel. The most common use of turboshaft engines is in scenarios where high power and reliability are required within a small envelope of requirements for size and weight. Most helicopter, marine, and auxiliary power units applications take advantage of turboshaft configurations. In fact, the turboshaft plays a workhorse role in the aviation industry as much as it is does for industrial power generation. While conventional turbine jet propulsion is achieved through thrust generated by a hot and fast exhaust stream, turboshaft engines creates shaft power that drives one or more rotors on the vehicle. -
Beyond the Paths of Heaven the Emergence of Space Power Thought
Beyond the Paths of Heaven The Emergence of Space Power Thought A Comprehensive Anthology of Space-Related Master’s Research Produced by the School of Advanced Airpower Studies Edited by Bruce M. DeBlois, Colonel, USAF Professor of Air and Space Technology Air University Press Maxwell Air Force Base, Alabama September 1999 Library of Congress Cataloging-in-Publication Data Beyond the paths of heaven : the emergence of space power thought : a comprehensive anthology of space-related master’s research / edited by Bruce M. DeBlois. p. cm. Includes bibliographical references and index. 1. Astronautics, Military. 2. Astronautics, Military—United States. 3. Space Warfare. 4. Air University (U.S.). Air Command and Staff College. School of Advanced Airpower Studies- -Dissertations. I. Deblois, Bruce M., 1957- UG1520.B48 1999 99-35729 358’ .8—dc21 CIP ISBN 1-58566-067-1 Disclaimer Opinions, conclusions, and recommendations expressed or implied within are solely those of the authors and do not necessarily represent the views of Air University, the United States Air Force, the Department of Defense, or any other US government agency. Cleared for public release: distribution unlimited. ii Contents Chapter Page DISCLAIMER . ii OVERVIEW . ix PART I Space Organization, Doctrine, and Architecture 1 An Aerospace Strategy for an Aerospace Nation . 3 Stephen E. Wright 2 After the Gulf War: Balancing Space Power’s Development . 63 Frank Gallegos 3 Blueprints for the Future: Comparing National Security Space Architectures . 103 Christian C. Daehnick PART II Sanctuary/Survivability Perspectives 4 Safe Heavens: Military Strategy and Space Sanctuary . 185 David W. Ziegler PART III Space Control Perspectives 5 Counterspace Operations for Information Dominance . -
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 -
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. -
USAF USAF Weapons 2008 USAF Almanac by Susan H.H
Gallery of USAF USAF Weapons 2008 USAF Almanac By Susan H.H. Young Note: Inventory numbers are total active inventory figures as of Sept. 30, 2007. Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying missions over intercontinental range, then penetrating enemy defenses with the largest pay- load 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: 67. Unit Location: Dyess AFB, Tex., Ellsworth AFB, S.D., Edwards AFB, Calif. Contractor: Boeing; AIL Systems; General Electric. Power Plant: four General Electric F101-GE-102 turbo- fans, each 30,780 lb thrust. B-1B Lancer (Richard VanderMeulen) Accommodation: four, pilot, copilot, and two systems officers (offensive and defensive), on zero/zero ACES II ejection seats. B-1B. Initiated in 1981, the first production model of Unit Location: Whiteman AFB, Mo. Dimensions: span spread 137 ft, swept aft 79 ft, length the improved variant B-1 flew in October 1984. USAF Contractor: Northrop Grumman; Boeing; Vought. 146 ft, height 34 ft. produced a total of 100. The active B-1B inventory was Power Plant: four General Electric F118-GE-100 turbo- Weights: empty equipped 192,000 lb, max operating reduced to 67 aircraft (from the remaining 92) with con- fans, each 17,300 lb thrust. weight 477,000 lb. solidation to two main operating bases within Air Combat Accommodation: two, mission commander and pilot, Ceiling: more than 30,000 ft. -
IMTEC-89-53 Military Space Operations: Use of Mobile Ground
. -. ,(. ,. .“” ,Y .,, . -- II, ./, .I i /, . % . ,L. United States Gdneral Accounting Off& Report to the Honorable &.A0 John P. Murtha, Chairman, Subcommittee on Defense, Committee on Appropriations, House of Representatives July 1989 MILITARY SPACE ’ OPERATIONS Use of Mobile Ground Stations in Satellite Control GAO/IMTEC439-63 United States General Accounting Office GAO Washington, D.C. 20548 Information Management and Technology Division B-224148 July 3, 1989 The Honorable John P. Murtha Chairman, Subcommittee on Defense Committee on Appropriations House of Representatives Dear Mr. Chairman: In your January 9, 1989, letter and in subsequent discussions with your office, you asked us to determine (1) how mobile ground stations fit into the Air Force’s overall satellite control architecture, (2) how many sta- tions exist and are planned, (3) what they cost by program element and appropriation account, and (4) how much the Department of Defense budgeted in fiscal year 1990 for mobile ground stations. As agreed with your office, our review focused primarily on mobile ground stations used by the Air Force’s satellite programs and included mobile ground stations used for one Defense Communications Agency satellite program. The Air Force’s satellite control architecture establishes a requirement for mobile ground stations to provide command and control instructions to maintain the position of a satellite in orbit as well as to provide the capability to process information coming from satellites. This network of stations, when completed, is planned to supplement fixed stations and/or to totally command and control a satellite’s position in orbit or process information. As of May 1989, there were 39 existing mobile ground stations. -
EASA AD No.: 2018-0211
EASA AD No.: 2018-0211 Airworthiness Directive AD No.: 2018-0211 Issued: 28 September 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation. This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption]. Design Approval Holder’s Name: Type/Model designation(s): CFM INTERNATIONAL S.A. CFM56-7B engines Effective Date: 05 October 2018 TCDS Number(s): EASA.E.004 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2018-0109 dated 17 May 2018. ATA 72 – Engine – Fan Blades – Inspection Manufacturer(s): SAFRAN Aircraft Engines, formerly SNECMA (France); General Electric Aircraft Engines (United States) Applicability: CFM56-7B20, CFM56-7B22, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B20/2, CFM56-7B22/2, CFM56-7B24/2, CFM56-7B26/2, -
Annex III to Decision 2015/029/R
AMC/GM TO ANNEX III (PART-66) TO REGULATION (EU) No 1321/2014 APPENDICES TO AMC TO PART-66 APPENDICES TO AMC TO PART-66 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCES The following aircraft type ratings should be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Regulation (EC) No 216/2008 and its Implementing Rules; this list is only intended for maintenance purposes. In order to keep this list current and the type ratings consistent, such information should be first passed on to the Agency using the Rulemaking Enquiry form (http://easa.europa.eu/webgate/rulemaking-enquiry/) in case a Member State needs to issue a type rating that is not included in this list. Notes on when the licences should be modified: When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the Aircraft Maintenance Licences (AMLs) may be modified at the next renewal or when the licence is reissued, unless there is an urgent reason to modify the licence. Notes on aircraft modified by Supplemental Type Certificate (STC): — This Appendix I intends to include the type ratings of aircraft resulting from STCs for installation of another engine. These STCs are those approved by the Agency and those approved by the Member States before 2003 and grandfathered by the Agency. -
Canada Aviation and Space Museum
CANADA AVIATION AND SPACE MUSEUM BOEING MODEL 720B PRATT & WHITNEY CANADA FLYING EXPERIMENTAL TEST BED REGISTRATION C-FETB Introduction The practical era of jet-age passenger transport aircraft officially dawned when the British de Havilland Company D.H.106 Comet made its premiere flight to great acclaim from the Hatfield, Hertfordshire aerodrome in England on 27 July 1949. Catering to British and mid to long-range routes to European, Middle Eastern and overseas destinations, the Comet series of airliners carried their passengers aloft in luxurious opulence for more than twenty years. Military and test derivatives followed suit and these continued flying for many decades, including two Comets for the Royal Canadian Air Force (RCAF). Just 14 days later, across the vast Atlantic Ocean, in the small town of Malton, Ontario, Canada, a new aviation company called Avro Canada successfully accomplished the same task with much less fanfare and accolades. Avro sent its small, medium-range, turbo-jet transport, called the C-102 Jetliner, aloft for its first flight, inaugurating the dreamed potential for such a unique travel experience for the public on the North American continent. United States Air Force personnel found the aircraft favourable when they tried it out on flights at Wright Field, Ohio in March 1951. However, this Canadian dream didn’t last for long. The modestly successful Comet-series didn’t shine as brightly as its popular name when a series of tragic, fatal accidents to production civil aircraft nearly snuffed out its very existence. Following design rectification’s, the Royal Air Force continued to employ Comets in versatile roles, such as modifying the design into the Nimrod.