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H. Con. Res. 122
IV 115TH CONGRESS 2D SESSION H. CON. RES. 122 Commemorating the 75th Anniversary of Lockheed Martin Skunk Works and its significant contributions to the national security of the United States. IN THE HOUSE OF REPRESENTATIVES JUNE 7, 2018 Mr. KNIGHT (for himself and Mr. COOK) submitted the following concurrent resolution; which was referred to the Committee on Armed Services CONCURRENT RESOLUTION Commemorating the 75th Anniversary of Lockheed Martin Skunk Works and its significant contributions to the national security of the United States. Whereas Lockheed Martin is known for building many of the finest military aircraft in the world; Whereas the Palmdale, California, location of Lockheed Mar- tin is headquarters to the Advanced Development Pro- grams group of the company, which is widely known as the ‘‘Skunk Works’’; Whereas the name the ‘‘Skunk Works’’— (1) came from ‘‘Li’l Abner’’, a satirical comic strip by Al Capp that was immensely popular in the 1940s and 1950s; (2) in 1943, was first used in reference to the Ad- vanced Development Programs group when the Depart- VerDate Sep 11 2014 02:15 Jun 08, 2018 Jkt 079200 PO 00000 Frm 00001 Fmt 6652 Sfmt 6300 E:\BILLS\HC122.IH HC122 dlhill on DSK3GLQ082PROD with BILLS 2 ment of the Navy attempted to establish a conference call connection and was mistakenly transferred to the XP–80 program of the Advanced Development Programs group, which due to classification could not be identified when the call was answered, and a member of the Advanced Development Programs group instead answered the call by saying, ‘‘Skunk Works’’, in reference to the location of the facility next to a malodorous plastics factory in Burbank, California; and (3) would later become the name that is used for the Advanced Development Programs group today, the ‘‘Skunk Works’’; Whereas the founding father of the Skunk Works was Clar- ence L. -
Concorde Is a Museum Piece, but the Allure of Speed Could Spell Success
CIVIL SUPERSONIC Concorde is a museum piece, but the allure Aerion continues to be the most enduring player, of speed could spell success for one or more and the company’s AS2 design now has three of these projects. engines (originally two), the involvement of Air- bus and an agreement (loose and non-exclusive, by Nigel Moll but signed) with GE Aviation to explore the supply Fourteen years have passed since British Airways of those engines. Spike Aerospace expects to fly a and Air France retired their 13 Concordes, and for subsonic scale model of the design for the S-512 the first time in the history of human flight, air trav- Mach 1.5 business jet this summer, to explore low- elers have had to settle for flying more slowly than speed handling, followed by a manned two-thirds- they used to. But now, more so than at any time scale supersonic demonstrator “one-and-a-half to since Concorde’s thunderous Olympus afterburn- two years from now.” Boom Technology is working ing turbojets fell silent, there are multiple indi- on a 55-seat Mach 2.2 airliner that it plans also to cations of a supersonic revival, and the activity offer as a private SSBJ. NASA and Lockheed Martin appears to be more advanced in the field of busi- are encouraged by their research into reducing the ness jets than in the airliner sector. severity of sonic booms on the surface of the planet. www.ainonline.com © 2017 AIN Publications. All Rights Reserved. For Reprints go to Shaping the boom create what is called an N-wave sonic boom: if The sonic boom produced by a supersonic air- you plot the pressure distribution that you mea- craft has long shaped regulations that prohibit sure on the ground, it looks like the letter N. -
Ovrhyp, Scramjet Test Aircraft STATE UNIVERSITY Student Authors: J
https://ntrs.nasa.gov/search.jsp?R=19910000728 2020-03-19T20:21:21+00:00Z /z7 H OVRhyp, Scramjet Test Aircraft STATE UNIVERSITY Student Authors: J. Asian, T. Bisard, S. Dallinga, K. Draper, G. Hufford, W. Peters, and J. Rogers Supervisor: Dr. G. M. Gregorek Assistant: R. L. Reuss Department of Aeronautical & Astronautical Engineering Universities Space Research Association Houston, Texas 77058 Subcontract Dated November 17, 1989 Final Report May 1990 03/0_ OVRhyp, Scramjet Test Aircraft UNIVERSITY Student Authors: J. Asian, T. Bisard, S. Dallinga, K. Draper, G. Hufford, W. Peters, and J. Rogers Supervisor: Dr. G. M. Gregorek Assistant: R. L. Reuss Department of Aeronautical & Astronautical Engineering Universities Space Research Association Houston, Texas 77058 Subcontract Dated November 17, 1989 Final Report RF Project 767919/722941 May 1990 ABSTRACT (Gary Huff0rd} A preliminary design for an unmanned hypersonic research vehicle to test scramjet engines is presented. The aircraft will be launched from a carrier aircraft at an altitude of 4Q,0QQ feet at Mach 0.8. The vehicle will then accelerate to Mach 6 at an altitude of 100,000 feet. At this stage the prototype scramjet will be employed to accelerate the vehicle to Mach 10 and maintain Mach IQ flight for 2 minutes. The aircraft will then decelerate and safely land, presumably at NASA Dryden F[i_ht Test Center. ii TABLE OF CONTENTS ABSTRACT ............................ ii TABLE OF CONTENTS ....................... iii LIST OF FIGURES ......................... v INTRODUCTION .......................... vi CONFIGURATION .......................... WEIGHTS ANALYSIS ........................ 12 PURPOSE ............................. 12 METHOD ........................... 12 SYSTEMS .......................... 14 AERODYNAMIC SURFACES .................... 14 BODY STRUCTURE ....................... 15 THERMAL PROTECTION SYSTEM ................. 15 LAUNCH AND LANDING SYSTEM ................ -
United States Air Force and Its Antecedents Published and Printed Unit Histories
UNITED STATES AIR FORCE AND ITS ANTECEDENTS PUBLISHED AND PRINTED UNIT HISTORIES A BIBLIOGRAPHY EXPANDED & REVISED EDITION compiled by James T. Controvich January 2001 TABLE OF CONTENTS CHAPTERS User's Guide................................................................................................................................1 I. Named Commands .......................................................................................................................4 II. Numbered Air Forces ................................................................................................................ 20 III. Numbered Commands .............................................................................................................. 41 IV. Air Divisions ............................................................................................................................. 45 V. Wings ........................................................................................................................................ 49 VI. Groups ..................................................................................................................................... 69 VII. Squadrons..............................................................................................................................122 VIII. Aviation Engineers................................................................................................................ 179 IX. Womens Army Corps............................................................................................................ -
Air Force Sexual Assault Court-Martial Summaries 2010 March 2015
Air Force Sexual Assault Court-Martial Summaries 2010 March 2015 – The Air Force is committed to preventing, deterring, and prosecuting sexual assault in its ranks. This report contains a synopsis of sexual assault cases taken to trial by court-martial. The information contained herein is a matter of public record. This is the final report of this nature the Air Force will produce. All results of general and special courts-martial for trials occurring after 1 April 2015 will be available on the Air Force’s Court-Martial Docket Website (www.afjag.af.mil/docket/index.asp). SIGNIFICANT AIR FORCE SEXUAL ASSAULT CASE SUMMARIES 2010 – March 2015 Note: This report lists cases involving a conviction for a sexual assault offense committed against an adult and also includes cases where a sexual assault offense against an adult was charged and the member was either acquitted of a sexual assault offense or the sexual assault offense was dismissed, but the member was convicted of another offense involving a victim. The Air Force publishes these cases for deterrence purposes. Sex offender registration requirements are governed by Department of Defense policy in compliance with federal and state sex offender registration requirements. Not all convictions included in this report require sex offender registration. Beginning with July 2014 cases, this report also indicates when a victim was represented by a Special Victims’ Counsel. Under the Uniform Code of Military Justice, sexual assaults against those 16 years of age and older are charged as crimes against adults. The appropriate disposition of sexual assault allegations and investigations may not always include referral to trial by court-martial. -
Technology Innovation and the Future of Air Force Intelligence Analysis
C O R P O R A T I O N LANCE MENTHE, DAHLIA ANNE GOLDFELD, ABBIE TINGSTAD, SHERRILL LINGEL, EDWARD GEIST, DONALD BRUNK, AMANDA WICKER, SARAH SOLIMAN, BALYS GINTAUTAS, ANNE STICKELLS, AMADO CORDOVA Technology Innovation and the Future of Air Force Intelligence Analysis Volume 2, Technical Analysis and Supporting Material RR-A341-2_cover.indd All Pages 2/8/21 12:20 PM For more information on this publication, visit www.rand.org/t/RRA341-2 Library of Congress Cataloging-in-Publication Data is available for this publication. ISBN: 978-1-9774-0633-0 Published by the RAND Corporation, Santa Monica, Calif. © Copyright 2021 RAND Corporation R® is a registered trademark. Cover: U.S. Marine Corps photo by Cpl. William Chockey; faraktinov, Adobe Stock. Limited Print and Electronic Distribution Rights This document and trademark(s) contained herein are protected by law. This representation of RAND intellectual property is provided for noncommercial use only. Unauthorized posting of this publication online is prohibited. Permission is given to duplicate this document for personal use only, as long as it is unaltered and complete. Permission is required from RAND to reproduce, or reuse in another form, any of its research documents for commercial use. For information on reprint and linking permissions, please visit www.rand.org/pubs/permissions. The RAND Corporation is a research organization that develops solutions to public policy challenges to help make communities throughout the world safer and more secure, healthier and more prosperous. RAND is nonprofit, nonpartisan, and committed to the public interest. RAND’s publications do not necessarily reflect the opinions of its research clients and sponsors. -
Some Supersonic Aerodynamics
Some Supersonic Aerodynamics W.H. Mason Configuration Aerodynamics Class Grumman Tribody Concept – from 1978 Company Calendar The Key Topics • Brief history of serious supersonic airplanes – There aren’t many! • The Challenge – L/D, CD0 trends, the sonic boom • Linear theory as a starting point: – Volumetric Drag – Drag Due to Lift • The ac shift and cg control • The Oblique Wing • Aero/Propulsion integration • Some nonlinear aero considerations • The SST development work • Brief review of computational methods • Possible future developments Are “Supersonic Fighters” Really Supersonic? • If your car’s speedometer goes to 120 mph, do you actually go that fast? • The official F-14A supersonic missions (max Mach 2.4) – CAP (Combat Air Patrol) • 150 miles subsonic cruise to station • Loiter • Accel, M = 0.7 to 1.35, then dash 25nm – 4 ½ minutes and 50nm total • Then, head home or to a tanker – DLI (Deck Launch Intercept) • Energy climb to 35K ft., M = 1.5 (4 minutes) • 6 minutes at 1.5 (out 125-130nm) • 2 minutes combat (slows down fast) After 12 minutes, must head home or to a tanker Very few real supersonic airplanes • 1956: the B-58 (L/Dmax = 4.5) – In 1962: Mach 2 for 30 minutes • 1962: the A-12 (SR-71 in ’64) (L/Dmax = 6.6) – 1st supersonic flight, May 4, 1962 – 1st flight to exceed Mach 3, July 20, 1963 • 1964: the XB-70 (L/Dmax = 7.2) – In 1966: flew Mach 3 for 33 minutes • 1968: the TU-144 – 1st flight: Dec. 31, 1968 • 1969: the Concorde (L/Dmax = 7.4) – 1st flight, March 2, 1969 • 1990: the YF-22 and YF-23 (supercruisers) – YF-22: 1st flt. -
Department of Defense Office of the Secretary
Monday, May 16, 2005 Part LXII Department of Defense Office of the Secretary Base Closures and Realignments (BRAC); Notice VerDate jul<14>2003 10:07 May 13, 2005 Jkt 205001 PO 00000 Frm 00001 Fmt 4717 Sfmt 4717 E:\FR\FM\16MYN2.SGM 16MYN2 28030 Federal Register / Vol. 70, No. 93 / Monday, May 16, 2005 / Notices DEPARTMENT OF DEFENSE Headquarters U.S. Army Forces Budget/Funding, Contracting, Command (FORSCOM), and the Cataloging, Requisition Processing, Office of the Secretary Headquarters U.S. Army Reserve Customer Services, Item Management, Command (USARC) to Pope Air Force Stock Control, Weapon System Base Closures and Realignments Base, NC. Relocate the Headquarters 3rd Secondary Item Support, Requirements (BRAC) U.S. Army to Shaw Air Force Base, SC. Determination, Integrated Materiel AGENCY: Department of Defense. Relocate the Installation Management Management Technical Support ACTION: Notice of Recommended Base Agency Southeastern Region Inventory Control Point functions for Closures and Realignments. Headquarters and the U.S. Army Consumable Items to Defense Supply Network Enterprise Technology Center Columbus, OH, and reestablish SUMMARY: The Secretary of Defense is Command (NETCOM) Southeastern them as Defense Logistics Agency authorized to recommend military Region Headquarters to Fort Eustis, VA. Inventory Control Point functions; installations inside the United States for Relocate the Army Contracting Agency relocate the procurement management closure and realignment in accordance Southern Region Headquarters to Fort and related support functions for Depot with Section 2914(a) of the Defense Base Sam Houston. Level Reparables to Aberdeen Proving Ground, MD, and designate them as Closure and Realignment Act of 1990, as Operational Army (IGPBS) amended (Pub. -
“Keep the Dream Alive”
February 28, 2015 The 60th Annual Honors and Awards Banquet “Keep the Dream Alive” February 28, 2015 th 60 Honors & Awards Banquet Diamond Anniversary 1 The 60th Annual Honors and Awards Banquet February 28, 2015 National Engineers Week Committees ~ BANQUET COMMITTEE ~ Kenneth Davis, Sonja Domazet, Stephen Guine, William Johnson, Sharlene Katz, Paul Landry, Robert Tarn, Thomas R. Tarn, Charles Volk ~ HONORS & AWARDS COMMITTEE ~ Marek Barylak, Kenneth Davis, Stephen Guine, Sharlene Katz, Paul Landry, Charles Olsefsky, R. Freeman Straub, Robert B. Tarn ~ AWARDS ASSEMBLY ~ Ken Davis, Sonja Domazet, James Flynn, Bill Johnson, Sharlene Katz, Charles Olsefsky ~ HOST / HOSTESSES ~ Olivia Landry, Maria Tarn ~ SOUVENIR PROGRAM GRAPHICS & DESIGN ~ Paul Landry ~ AWARD GRAPHICS ~ Mike Matte ~ AUDIO / VIDEO ~ Swank Audio Visuals, Carlos Guerra ~ BANQUET SETUP / AWARDS DISTRIBUTION ~ Marissa Bayless, Margo Guerra ~ MATH COUNTS ~ Jerry Kraim, Eli Stiny Engineers’ Council Past Presidents 1970 William B. Johnson 1992 Robert Budica 2005 Robert B. Tarn 1980 Clifford B. Shiepe, PE 1993 Lloyd W. Higginbotham, FIAE 2006 Paul F. Landry 1981 Clifford B. Shiepe, PE 1994 Lloyd W. Higginbotham, FIAE 2007 Paul F. Landry 1982 Lloyd W. Higginbotham, FIAE 1995 Lloyd W. Higginbotham, FIAE 2008 Patrick Berbon 1983 William F. Hassel, PE, FIAE 1996 Lloyd W. Higginbotham, FIAE 2009 Dr. Charles H. Volk 1984 Clifford Terry 1997 Lloyd W. Higginbotham, FIAE 2010 Dr. Charles H. Volk 1985 Roland V. Roggero 1998 Lloyd W. Higginbotham, FIAE 2011 Kenneth G. Davis 1986 James P. Ritchey 1999 Lloyd W. Higginbotham, FIAE 2012 Kenneth G. Davis 1987 James P. Ritchey 2000 Lloyd W. Higginbotham, FIAE 2013 Sonja Domazet 1988 Harlan L. Russ 2001 Lloyd W. -
Download Chapter 155KB
Memorial Tributes: Volume 8 BEN RICH 200 Copyright National Academy of Sciences. All rights reserved. Memorial Tributes: Volume 8 BEN RICH 201 Ben Rich 1925-1995 By Willis M. Hawkins Ben Rich died on January 5, 1995, after a full career as an engineer, a designer, and an effective and cherished executive. I first knew Ben when he joined the Lockheed Aircraft Company in Burbank back in 1950. He came to us from the University of California, Berkeley, and University of California, Los Angeles, with a master's degree in mechanical engineering. At the time, I was in charge of the Advanced Design Organization under the Deputy Chief Engineer C. L. "Kelly" Johnson, and we were working on our first Mach 2+ Air Force fighter proposal, which became the F-104. Ben was assigned the task of analyzing the aerothermodynamic performance of the power plant with little or no existing state of the art for supersonic inlets. It is a testament to Ben's understanding of this specialty that the inlet configuration was classified by the Air Force and the details obscured in Air Force-released pictures of the airplane for a number of years. The Lockheed "Skunk Works," which had originated during the design and development of the original P-80 prototype "Lulu-Belle," was being reactivated at about the time that the F-104 was conceived. Its specific purpose was the secret development of the U-2, and Ben was ''borrowed" by Kelly Johnson to help on that program. His "temporary'' assignment became his career. Under Kelly, Ben pursued his specialty of aerothermodynamic analysis. -
National Reconnaissance Office Review and Redaction Guide
NRO Approved for Release 16 Dec 2010 —Tep-nm.T7ymqtmthitmemf- (u) National Reconnaissance Office Review and Redaction Guide For Automatic Declassification Of 25-Year-Old Information Version 1.0 2008 Edition Approved: Scott F. Large Director DECL ON: 25x1, 20590201 DRV FROM: NRO Classification Guide 6.0, 20 May 2005 NRO Approved for Release 16 Dec 2010 (U) Table of Contents (U) Preface (U) Background 1 (U) General Methodology 2 (U) File Series Exemptions 4 (U) Continued Exemption from Declassification 4 1. (U) Reveal Information that Involves the Application of Intelligence Sources and Methods (25X1) 6 1.1 (U) Document Administration 7 1.2 (U) About the National Reconnaissance Program (NRP) 10 1.2.1 (U) Fact of Satellite Reconnaissance 10 1.2.2 (U) National Reconnaissance Program Information 12 1.2.3 (U) Organizational Relationships 16 1.2.3.1. (U) SAF/SS 16 1.2.3.2. (U) SAF/SP (Program A) 18 1.2.3.3. (U) CIA (Program B) 18 1.2.3.4. (U) Navy (Program C) 19 1.2.3.5. (U) CIA/Air Force (Program D) 19 1.2.3.6. (U) Defense Recon Support Program (DRSP/DSRP) 19 1.3 (U) Satellite Imagery (IMINT) Systems 21 1.3.1 (U) Imagery System Information 21 1.3.2 (U) Non-Operational IMINT Systems 25 1.3.3 (U) Current and Future IMINT Operational Systems 32 1.3.4 (U) Meteorological Forecasting 33 1.3.5 (U) IMINT System Ground Operations 34 1.4 (U) Signals Intelligence (SIGINT) Systems 36 1.4.1 (U) Signals Intelligence System Information 36 1.4.2 (U) Non-Operational SIGINT Systems 38 1.4.3 (U) Current and Future SIGINT Operational Systems 40 1.4.4 (U) SIGINT -
Goatsucker: Toward a Spatial Theory of State Secrecy
Environment and Planning D: Society and Space 2010, volume 28, pages 759 ^ 771 doi:10.1068/d5308 Goatsucker: toward a spatial theory of state secrecy Trevor Paglen Department of Geography, University of California at Berkeley, 507 McCone Hall #4740, Berkeley, CA 94720, USA; e-mail: [email protected] Received 1 May 2008; in revised form 6 April 2010 Abstract. While the question of state secrecy has become a topic of much political debate, relatively little attention has been paid to the topic in academic literature. Most of the literature adopts one of several frameworks. In the legal literature, state secrecy has been examined as a historical and constitutional question. Social scientists have tended to follow Weber in examining secrecy as a question of regulation and bureaucracy or have focused on the cultural play of visibility and invisi- bility that is often characteristic of state secrecy. This paper, by way of contrast, uses the development of the F-117A `stealth fighter' as a case study to give a spatial account of secrecy. I show how state secrecy gives rise to numerous spatial, political, juridical, and even ecological contradictions and propose that a spatial understanding of state secrecy foregrounding these contradictions provides a fruitful basis for a deeper understanding of state secrecy. Late one night during the summer of 1984, two fighter pilots saw a ghost in the sky above Las Vegas. A single two-seat F-16 `Viper' fighter was on a routine flight over the city that night, its pilots alternating between watching instruments, checking in with ground controllers, and scanning the skies above.