Fundamentals of Guided Missiles Fundamentals of Guided Missiles
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DRDO Successfully Tests Armour-Piercing Nag Missiles At
Tue, 09 July 2019 DRDO successfully tests armour-piercing Nag Missiles at Pokhran range The Defence Acquisition Council in 2018 had approved the procurement of DRDO designed and developed NAG Missile System (NAMIS) at a cost of Rs 524 crore New Delhi: Moving closer toward the induction of the Nag anti-tank guided missiles into the Army, Defence Research and Development Organisation (DRDO) on Sunday carried out three successful test firings of the missiles in the Pokhran firing ranges. "The missiles were test-fired during both day and night on Sunday during the trials. All three tests were successful," DRDO officials said. Government sources said the missile is in the final stages of being inducted into the Army which will use it by mounting them on modified armoured vehicles. The Defence Acquisition Council in 2018 had approved the procurement of DRDO-designed- and-developed NAG Missile System (NAMIS) at a cost of Rs 524 crore. The system includes a third-generation Anti-Tank Guided Missile, the NAG, along with the Missile Carrier Vehicle (NAMICA). The NAG missile is a third-generation anti-tank guided missile, which has top attack capabilities that can effectively engage and destroy all known enemy tanks during both day and night operations. The successful induction of NAG missile into the Army is expected to give a quantum boost to the Army's capability against enemy armour. NAG was one of the first five strategic missiles planned to be developed under the Integrated Missile Development Programme initiated in the 1980s. The other missiles developed under the project include Agni, Prithvi and Akash, and all three have been successfully developed and inducted into the armed forces. -
0 January to July 2021
0 www.journalsofindia.com January to July 2021 SCIENCE & TECH ............................................................................................................................................................... 6 1. REUSABLE LAUNCH VEHICLE TECHNOLOGY DEMONSTRATION PROGRAMME(RLV-TD) ................................................. 6 2. GAGANYAAN MISSION ..................................................................................................................................................... 6 3. MARS ORBITER MISSION (MOM) ..................................................................................................................................... 6 4. CHANDRAYAAN MISSION................................................................................................................................................. 7 5. SOLAR MISSION ............................................................................................................................................................... 8 6. ARTEMIS ACCORD ............................................................................................................................................................ 9 7. NATIONAL MISSION ON INTERDISCIPLINARY CYBER-PHYSICAL SYSTEM (NMICPS) ....................................................... 10 8. SMART ANTI-AIRFIELD WEAPON (SAAW) ...................................................................................................................... 10 9. AQUAPONICS ................................................................................................................................................................ -
Prepared by Textore, Inc. Peter Wood, David Yang, and Roger Cliff November 2020
AIR-TO-AIR MISSILES CAPABILITIES AND DEVELOPMENT IN CHINA Prepared by TextOre, Inc. Peter Wood, David Yang, and Roger Cliff November 2020 Printed in the United States of America by the China Aerospace Studies Institute ISBN 9798574996270 To request additional copies, please direct inquiries to Director, China Aerospace Studies Institute, Air University, 55 Lemay Plaza, Montgomery, AL 36112 All photos licensed under the Creative Commons Attribution-Share Alike 4.0 International license, or under the Fair Use Doctrine under Section 107 of the Copyright Act for nonprofit educational and noncommercial use. All other graphics created by or for China Aerospace Studies Institute Cover art is "J-10 fighter jet takes off for patrol mission," China Military Online 9 October 2018. http://eng.chinamil.com.cn/view/2018-10/09/content_9305984_3.htm E-mail: [email protected] Web: http://www.airuniversity.af.mil/CASI https://twitter.com/CASI_Research @CASI_Research https://www.facebook.com/CASI.Research.Org https://www.linkedin.com/company/11049011 Disclaimer The views expressed in this academic research paper are those of the authors and do not necessarily reflect the official policy or position of the U.S. Government or the Department of Defense. In accordance with Air Force Instruction 51-303, Intellectual Property, Patents, Patent Related Matters, Trademarks and Copyrights; this work is the property of the U.S. Government. Limited Print and Electronic Distribution Rights Reproduction and printing is subject to the Copyright Act of 1976 and applicable treaties of the United States. This document and trademark(s) contained herein are protected by law. This publication is provided for noncommercial use only. -
Winning the Salvo Competition Rebalancing America’S Air and Missile Defenses
WINNING THE SALVO COMPETITION REBALANCING AMERICA’S AIR AND MISSILE DEFENSES MARK GUNZINGER BRYAN CLARK WINNING THE SALVO COMPETITION REBALANCING AMERICA’S AIR AND MISSILE DEFENSES MARK GUNZINGER BRYAN CLARK 2016 ABOUT THE CENTER FOR STRATEGIC AND BUDGETARY ASSESSMENTS (CSBA) The Center for Strategic and Budgetary Assessments is an independent, nonpartisan policy research institute established to promote innovative thinking and debate about national security strategy and investment options. CSBA’s analysis focuses on key questions related to existing and emerging threats to U.S. national security, and its goal is to enable policymakers to make informed decisions on matters of strategy, security policy, and resource allocation. ©2016 Center for Strategic and Budgetary Assessments. All rights reserved. ABOUT THE AUTHORS Mark Gunzinger is a Senior Fellow at the Center for Strategic and Budgetary Assessments. Mr. Gunzinger has served as the Deputy Assistant Secretary of Defense for Forces Transformation and Resources. A retired Air Force Colonel and Command Pilot, he joined the Office of the Secretary of Defense in 2004. Mark was appointed to the Senior Executive Service and served as Principal Director of the Department’s central staff for the 2005–2006 Quadrennial Defense Review. Following the QDR, he served as Director for Defense Transformation, Force Planning and Resources on the National Security Council staff. Mr. Gunzinger holds an M.S. in National Security Strategy from the National War College, a Master of Airpower Art and Science degree from the School of Advanced Air and Space Studies, a Master of Public Administration from Central Michigan University, and a B.S. in chemistry from the United States Air Force Academy. -
Missiles OUTLOOK
SPECIFICATIONS Missiles OUTLOOK/ GENERAL DATA AIRFRAME GUIDANCE OUTLOOK/ POWERPLANT SPECIFICATIONS MAX. MAX. SPAN, BODY LAUNCH MAX. RANGE STATUS/OUTLOOK/REMARKS DESIGNATION/NAME LENGTH WINGS OR DIAMETER WEIGHT CONTRACTOR TYPE NO. MAKE & MODEL (FT.) FINS (FT.) (FT.) (LB.) (NAUT. MI.) AIR-TO-AIR CHUNG-SHAN INSTITUTE OF SCIENCE AND TECHNOLOGY (CSIST), Taoyuan, Taiwan Skysword 1 (Tien Chien 1) 9.8 2.1 0.42 196.4 — IR 1 X solid propellant 9.7 In service with Taiwan air force since 1993. Skysword 2 (Tien Chien 2) 11.8 2 0.62 396.8 — Active radar 1 X solid propellant 32.4 In service with Taiwan air force since 1996. DENEL (PTY.) LTD., Pretoria, South Africa OPERATORS SATELLITE A-Darter 9.8 1.6 0.54 195.8 Denel IIR 1 X solid propellant — Fifth-generation technology demonstrator. Likely co-development with Brazil. COMMERCIAL R-Darter 11.9 2.1 0.53 264 Denel Radar 1 X solid propellant — Development completed 2000. For South African Air Force Cheetah and Gripen aircraft. U-Darter 9.6 1.67 0.42 210 Denel Two-color, IR 1 X solid propellant — First revealed in 1988; similar to Magic. Entered production in 1994. In use on South African Air Force Cheetah and Impala aircraft. DIEHL BGT DEFENSE, Uberlingen, Germany COMMERCIAL AIM-9L/I-1 Sidewinder 9.4 2.1 0.4 189 Diehl BGT Defense IR 1 X solid propellant — Upgraded and refurbished. IRIS-T 9.7 — 0.4 196 Diehl BGT Defense IIR 1 X solid propellant — In production. SATELLITE OPERATORS SATELLITE MBDA MISSILE SYSTEMS (BAE Systems, EADS, Finmeccanica), London, UK; Vélizy, France; Rome, Italy Aspide 12.1 3.4 0.67 479 Alenia Semiactive radar, homing 1 X solid propellant 43 In service. -
Spacecraft Guidance Techniques for Maximizing Mission Success
Utah State University DigitalCommons@USU All Graduate Theses and Dissertations Graduate Studies 5-2014 Spacecraft Guidance Techniques for Maximizing Mission Success Shane B. Robinson Utah State University Follow this and additional works at: https://digitalcommons.usu.edu/etd Part of the Mechanical Engineering Commons Recommended Citation Robinson, Shane B., "Spacecraft Guidance Techniques for Maximizing Mission Success" (2014). All Graduate Theses and Dissertations. 2175. https://digitalcommons.usu.edu/etd/2175 This Dissertation is brought to you for free and open access by the Graduate Studies at DigitalCommons@USU. It has been accepted for inclusion in All Graduate Theses and Dissertations by an authorized administrator of DigitalCommons@USU. For more information, please contact [email protected]. SPACECRAFT GUIDANCE TECHNIQUES FOR MAXIMIZING MISSION SUCCESS by Shane B. Robinson A dissertation submitted in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY in Mechanical Engineering Approved: Dr. David K. Geller Dr. Jacob H. Gunther Major Professor Committee Member Dr. Warren F. Phillips Dr. Charles M. Swenson Committee Member Committee Member Dr. Stephen A. Whitmore Dr. Mark R. McLellan Committee Member Vice President for Research and Dean of the School of Graduate Studies UTAH STATE UNIVERSITY Logan, Utah 2013 [This page intentionally left blank] iii Copyright c Shane B. Robinson 2013 All Rights Reserved [This page intentionally left blank] v Abstract Spacecraft Guidance Techniques for Maximizing Mission Success by Shane B. Robinson, Doctor of Philosophy Utah State University, 2013 Major Professor: Dr. David K. Geller Department: Mechanical and Aerospace Engineering Traditional spacecraft guidance techniques have the objective of deterministically min- imizing fuel consumption. -
Former Warsaw Pact Ammunition Handbook, Vol 3
NATO Explosive Ordnance Disposal Centre of Excellence FORMER WARSAW PACT AMMUNITION HANDBOOK VOLUME 3 Air Forces Ammunition Aerial projectiles, bombs, rockets and missiles TRENČÍN 2019 Slovak Republic For Official Use Only Explosive Ordnance Disposal Centre of Excellence FORMER WARSAW PACT AMMUNITION HANDBOOK VOLUME 3 Air Forces Ammunition Aerial projectiles, bombs, rockets and missiles For Official Use Only Explosive Ordnance Disposal Centre of Excellence The NATO Explosive Ordnance Centre of Excellence (NATO EOD COE) supports the efforts of the Alliance in the areas of training and education, information sharing, doctrine development and concepts validation. Published by NATO EOD Centre of Excellence Ivana Olbrachta 5, 911 01,Trenčín, Slovak Republic Tel. + 421 960 333 502, Fax + 421 960 333 504 www.eodcoe.org Former Warsaw Pact Ammunition Handbook VOL 3 – Edition II. ISBN 978-80-89261-81-9 © EOD Centre of Excellence. All rights reserved 2019 No part of this book may be used or reproduced in any manner without the written permission of the publisher, except in the case brief quotations embodied in articles and reviews. For Official Use Only Explosive Ordnance Disposal Centre of Excellence Foreword Even though in areas of current NATO operations the insurgency is vastly using the Home Made Explosive as the main charge for emplaced IEDs, our EOD troops have to cope with the use of the conventional munition in any form and size all around the world. To assist in saving EOD Operators’ lives and to improve their effectiveness at munition disposal, it is essential to possess the adequate level of experience and knowledge about the respective type of munition. -
India's Missile Programme and Odisha : a Study
January - 2015 Odisha Review India's Missile Programme and Odisha : A Study Sai Biswanath Tripathy India’s missile and nuclear weapons programs First, there must be an open, uninhabited stretch have evolved as elements of its strategic response of land or water (several hundred kilometers long) to 68 years of wars and skirmishes it has fought ‘down range.’ Second, the site ideally, must allow with Pakistan and with China. Deep tensions and for longitudinal launch. The first requirement is to mistrust in the sub-continent continue unabated ensure that a malfunction during the launch stage to the present. India’s defeat by China in the 1962 does not cause damage to civilian lives and border war, probably more than any other event, property. Rocket propellant is highly explosive galvanized its leadership to build indigenous missile and if it does explode during the launch stage, and “threshold” nuclear weapons capabilities as burning fuel and metal fragments are sprayed over a credible deterrent against attack by China, and vast areas. Often, rockets fail to take off along to attain military superiority over Pakistan. the planned trajectory and have to be destroyed by the range safety officer. In this case too, the As far back as in November 1978, the· effects are so devastating that most launch sites government had set up a Committee to identify a around the world are consequently located on a site for the establishment of an instrumented test coast. range. A group of experts had surveyed a number The Bay of Bengal provides an ideal of sites, including the Sunderbans (West Bengal), stretch of sea over which missiles can be fired. -
Missile Guidance and Control
CHAPTER 4 MISSILE GUIDANCE AND CONTROL INTRODUCTION in the interest of terminology standardization and to assist common understanding, we shall call the In the preceding chapters you learned that the complete system within a missile that steers and essential parts a guided missile needs to perform stabilizes it a guidance and control system. properly are: Depending on your experience with missiles, you 1. Airframe and control surfaces. may take exception to this designation. And if you 2. Propulsion system. do, there is good reason for it. The reason is shown 3. Warhead system. in figure 4-1. For example, if you have worked on 4. Guidance and control system. the Tartar or Terrier missiles you will consider the In addition, in chapter 2 you studied the basic fire system that guides and controls a missile to be its control problem, and learned how some of the steering system. On the other hand, a Talos GMM forces of nature affect the trajectory of a guided would call it a guidance and control system. We missile as it flies to its intended target. In chapter 3 will stick with the latter designation - not because you learned how wings and fins steer a missile and we favor Talos but because most manuals, and keep it pointed along its flight path. The use of many Navy publications, use this term. interior control devices by missiles without exterior control surfaces (or limited ones) was described SUBSYSTEMS AND COMPONENTS briefly. The different types of guidance systems used in missiles are inertial, command, beam-rider, In figure 4-2 we show that the complete system and homing guidance. -
IJESRT INTERNATIONAL JOURNAL of ENGINEERING SCIENCES & RESEARCH TECHNOLOGY a LITERATURE STUDY on COMMAND to LINE of SIGHT MISSILE SYSTEM Ramakrishna G*1, G.K.D
ISSN: 2277-9655 [Ramakrishna* et al., 7(1): January, 2018] Impact Factor: 5.164 IC™ Value: 3.00 CODEN: IJESS7 IJESRT INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY A LITERATURE STUDY ON COMMAND TO LINE OF SIGHT MISSILE SYSTEM Ramakrishna G*1, G.K.D. Prasanna Venkatesan 2 * Faculty of ECE, Indian Naval Academy, Ezhimala, India DOI: 10.5281/zenodo.1147484 ABSTRACT The aim of this paper is to explain the CLOS (Command to Line of Sight) Missile Systems in detail. The includes the concept behind it, the technology used and the applications in modern warfare. While the paper will largely deal with CLOS guidance, the theory behind basic functioning of a guided weapon/missile will also be discussed. The MCLOS (Manual Command to Line of Sight), SACLOS (Semi Automatic Command to Line of Sight), and ACLOS (Automatic Command to Line of Sight) are also presented along with their applications. KEYWORDS: ACLOS, MCLOS, SACLOS I. INTRODUCTION A Guided weapon may be described briefly as a weapon system which the warhead is delivered by an unmanned guided vehicle. Guided missiles have only been in practical use since the advent of World War II. It is because the technology has enabled the invention of the final product has been around for a lot longer. From the oldest of discoveries, like that of gunpowder in the 1st millennium BC by the Chinese to the rapid advances in the field of science, they have all been required to the practical enabling of the concept of guided missile systems [1][2]. The Germans were the first to field guided weapons with the use of V1 guided bomb and the V2 rocket. -
Guidance, Navigation, and Control (GN&C) Efficient, Responsive, and Effective
Space Transportation Systems National Aeronautics and Space Administration Guidance, Navigation, and Control (GN&C) Efficient, Responsive, and Effective The GN&C capability is a critical enabler of • Navigation — system architecture trade every launch vehicle and spacecraft system. studies, sensor selection and modeling, posi- At-A-Glance Marshall applies a robust, responsive, team- tion/orientation determination software (filter) Guidance, navigation, and control capabilities oriented approach to the GN&C design, develop- development, architecture trade studies, auto- will be needed for today’s launch and tomor- ment, and test capabilities. From initial concept matic rendezvous and docking (AR&D), and row’s in-space applications. Marshall has through detailed mission analysis and design, Batch estimation — all mission phases. developed a GN&C capability with experience hardware development and test, verification and • Control — algorithms, vehicle and control directly supporting projects and serving as validation, and mission operations, the Center system requirements and specifications, a supplier and partner to industry, DOD, and can provide the complete end-to-end GN&C stability analyses, and controller design, academia. To achieve end-to-end develop- development and test — or provide any portion modeling and simulation. ment, this capability leverages tools such as of it — for launch vehicles or spacecraft systems the Flight Robotics Lab, specialized software • Sensor Hardware — selection, closed for any NASA mission. Recognized as the tools, and the portable SPRITE small satellite loop testing and qualification; design, build, Agency’s lead and a world-class developer of payload integration environment. The versatile and calibrate specialized sensors. Earth-to-orbit and in-space stages for GN&C, team also provides an anchor and resource Marshall is a key developer of in-space transpor- for government “smart buyer” oversight of tation, spacecraft control, automated rendezvous future space system acquisition, helping to and capture techniques, and testing. -
Ballistic Missile Defense Guidance and Control Issues
Science & Global Security, 1998, Volume 8, pp. 99-124 © 1998 OPA (Overseas Publishers Association) Reprints available directly from the publisher Amsterdam B.V. Photocopying permitted by license only Published under license by Gordon and Breach Science Publishers SA Printed in the United States of America Ballistic Missile Defense Guidance and Control Issues Paul Zarchana Ballistic targets can be more difficult to hit than aircraft targets. If the intercept takes place out of the atmosphere and if no maneuvering is taking place, the ballistic target motion can be fairly predictable since the only force acting on the target is that of grav- ity. In all cases an exoatmospheric interceptor will need fuel to maneuver in order to hit the target. The long engagement times will require guidance and control strategies which conserve fuel and minimize the acceleration levels for a successful intercept. If the intercept takes place within the atmosphere, the ballistic target is not as predict- able because asymmetries within the target structure may cause it to spiral. In addi- tion, the targets’ high speed means that very large decelerations will take place and appear as a maneuver to the pursuing endoatmospheric interceptor. In this case advanced guidance and control strategies are required to insure that the target can be hit even when the missile is out maneuvered. This tutorial will attempt to highlight the major guidance and control challenges facing ballistic missile defense. PREDICTING WHERE THE TARGET WILL BE Before an interceptor can be launched at a ballistic target, a sensor is first required to track the threat. For example, if the sensor is a ground radar, the range and angle from the radar to the target are measured.