Insensitive Munitions (Les Munitions a Risque Attgnu6)
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P--31 a5 db a AGARD ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 8 7 RUE ANCELLE 92200 NEUILLY SUR SEINE FRANCE AGARD CONFERENCE PROCEEDINGS 511 Insensitive Munitions (Les Munitions a Risque AttGnu6) Processed /not arocessed by DIMS ................................ signed.................. date * NOT FOR DESTRUCTION Papers presented at the Propulsion and Energetics Panel *. 78th A Spectalists’ Meeting held in Bonn, Germany, 21st-23rd October 1991. - <*> - NORTH ATLANTIC TREATY ORGANlZAnON 1 Published July 1992 Distribution and Availability on Back Cover . c ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE ANCELLE 92200 NEUILLY SUR SEINE FRANCE AGARD CONFERENCE PROCEEDINGS 511 Insensitive Munitions (Les Munitions B Risque Attknue) . Papers presented at the Propulsion and Energetics Panel . 78th A Specialists’ Meeting held in Bonn, Germany, 21st-23rd October 1991. - North Atlantic Treaty Organization \/- Organisation du Traite de I’Atlantique Nord I The Mission of AGARD . According to its Chartcr, thc mission of AGARD is to bring togethcr thc leading personalities of the NATO nations in t le fields of science and technology relating to aerospace for the following purposes: -Recommending effective ways for the member nations to use their research and development capabilities for the .. common benefit of the h'AT0 community; - Providing scientific and technical advice and assistancc to the Military Committee in the field of aerospace research and development (with particular regard to its military application); - Continuously stimulating advances in the aerospace sciences relevant to strengthening the common defence posture; - Improving the co-operation among member nations in aerospace research and development; -Exchange of scientific and technical information; - Providing assistance to member nations for the purpose of increasing their scientific and technical potential; - Rendering scientific and technical assistance, as requested, to other NATO bodies and to member nations in comiection with research and development problems in the aerospace field. e Thc highest authority within AGARD is the National Delegates Board consisting of olficially appointed senior representatives from each member nation. The mission of AGARD is carried out through the Panels which are composed of experts appointed by the National Delegates, the Consultant and Exchange Programme and the Aerospace Applications Studies Prograinn e. The results of AGARD work are reported to the member nations and the NATO Authorities through the AGARD series of publications of which this is one. Participetion in AGARD activities is by invitation only and is normally limited to citizens of the NATO nations, The content of this publication has bcen reproduced directly from material supplied by AGARD or the authors Published July 1992 Copyright 0 AGARD 1992 All Rights Reserved ISBN 92-835-0679-0 Printed by Speriulised Printing Services Limited 40 Chigwell Lune, Loughton, Essex IGI0 3TZ Recent Publications of the Propulsion and Energetics Panel - CONFERENCE PROCEEDINGS (CP) Combustion Problems in Turbine Engines ’+. AGARD CP 353, January 1984 Hazard Studies for Solid Propellant Rocket Motors AGARD CP 367, September 1984 Engine Cyclic Durability by Analysis and Testing AGARD CP 368, September 1984 Gears and Power Transmission Systems for Helicopters and Turboprops AGARD CP 369, January 1985 Heat Transfer and Cooling in Gas Turbines AGARD CP 390, September 1985 Smokeless Propellants AGARD CP 391, January 1986 Interior Ballistics of Guns AGARD CP 392, January 1986 Advanced Instrumentation for Aero Engine Components AGARD CP 399, November 1986 Engine Response to Distorted Inflow Conditions AGARD CP 400, March 1987 Transonic and Supersonic Phenomena in Turbomachines AGARDCP401,March 1987 Advanced Technology for Aero Engine Components AGARD CP 421, September 1987 Combustion and Fuels in Gas Turbine Engines AGARD CP 422, June 1988 Engine Condition Monitoring - Technology and Experience AGARD CP 448, October 1988 Application of Advanced Material for Turbomachinery and Rocket Propulsion AGARDCP449,March 1989 Combustion Instabilities in Liquid-Fuelled Propulsion Systems AGARD CP 450, April 1989 .I Aircraft Fire Safety AGARD CP 467, October 1989 * Unsteady Aerodynamic Phenomena in Turbomachines AGARD CP 468, February 1990 Secondary Flows in Turbomachines AGARD CP 469, February 1990 Hypersonic Combined Cycle Propulsion AGARD CP 479, December 1990 Low Temperature Environment Operations of Turboengines (Design and User’s Problems) AGARDCP480,May 1991 CFD Techniques for Propulsion Applications AGARD CP 510,February 1992 Combat Aircraft Noise AGARDCP512,ApriIlYY2 iii ADVISORY REPORTS (AR) Through Flow Calculations in Axial Turbomachines (Results of Working Group 12) AGARDAR 175,October 1981 Alternative Jet Engine Fuels (Results of Working Group IS) AGARDAR 181,Vol.l andVo1.2,July 1982 Suitable Averaging Techniques in Non-Uniform Internal Flows (Results of Working Group 14) AGARD AR 182 (in English and French), June/August 1983 Producibility and Cost Studies of Aviation Kerosines (Results of Working Group 16) AGARDAR227,June 1985 Performance of Rocket Motors with Metallized Propellants (Resultr of Working Group 17) AGARD AR 230, September 1986 Recommended Practices for Measurement of Gas Path Pressures and Temperatures for Performance Assessment of Aircraft Turbine Engines and Components (Results of Working Group 19) AGARD AR 245, June 1990 The Uniform Engine Test Programme (Results of Working Group IS) AGARD AR248,Febmary 1990 Test Cases for Computation oflnternal Flows in Aero Engine Components (Results of Working Group 18) AGARD AR 275, July 1990 LECTURE SERIES (LS) 3-D Computation Techniques Apptied to Internal Flows in Propulsion Systems AGARD LS 140, June 1985 Engine Airframe Integration for Rotorcraft AGARDLS 148, June 1986 Design Methods Used in Solid Rocket Motors AGARD LS 150, April 1987 AGARD LS 150 (Revised), April 1988 Blading Design for Axial Turbomachines AGARD LS 167, June 1989 Comparative Engine Performance Measurements AGARDLS 169,May 1990 Combustion of Solid Propellants AGARDLS 180,June 1991 Steady and Transient Performance Prediction of Gas Turbine Engines AGARD LS 183, May 1992 AGARDOGRAPHS (AG) Manual for Aeroelasticity in Turbomachines AGARD AG 298/1, March 1987 AGARD AG 298/2, June 1988 Measurement Uncertainty within the Uniform Engine Test Programme AGARD AG 307, May 1989 Hazard Studies for Solid Propellant Rocket Motors AGARDAG316,September 1990 REPORTS (R) Application of Modified Loss and Deviation Correlations to Transonic Axial Compressors AGARD R 745, November 1987 Rotorcraft Drivetrain Life Safety and Reliability AGARD R 775, June 1990 Theme “Insensitive Munitions” is an important area to NATO in light of the recent initiative by CNAD to develop a NATO Insensitive Munitions Information Centre (NIMIC) in Brussels in 1991. Insensitive munition requirements, evolving in NATO and many individual nations, are aimed at reducing the potential for and effects of unintended activation of munitions caused by their exposure to environmental forces. Such forces can occur either normally in situations such as transport and storage, in accidents such as fire, or combat circumstances through impact from bullets and fragments. The scope of the meeting focused on hazard technologies associated with rocket propulsion but also included other munition components that would be included in an overall safety assessment of a missile system. The scope was: - requirements in NATO Nations - approaches for hazard assessment - studies on hazard threat areas - studies on hazard technology areas - development of new energetic material and - development of devices to reduce destructive response to stimuli. Theme “Les Munitions B Risque Att6nui”est un domaine dbormais important pour I’OTAN, suite a I’initiative prise par le CNAD visant a la criation d’un centre de renseignements OTAN sur les munitions a risque attinu6 (NIMIC) i BNxelles pour l’annee 1991. Les spicifications des munitions i risque attinu4 qui sont en cours dilaboration au sein de I’OTAN, ainsi que dans de nombreux pays, ont pour objet la reduction du potentiel et des effets de l‘amorcage involontaire des munitions suite a leur exposition aux forces externes. De telles forces se manifestent soit en temps normal, 101s des operations de transport et de stockage par exemple, soit en cas daccident tel qu’une incendie, soit en situation de combat lors de I‘impact de balles et declats. La rimion a mis l’accent sur les technologies du risque associees a la propulsion par fusee, tout en incluant les autres i16ments constitutifs du systime qui itaient prendre en compte lors de l‘kvaluation des risques present6 par un systime de missiles. La r&nion a examine les sujets suivants: - les besoins exprimes par les pays memhres de l’OTAN - les approches possibles de I‘evaluation du risque - les itudes sur les domaines a grand risque - les &tudessur les technologies du risque - le developpement de nouvelles matieres energetiques - le d6veloppement d‘appareils destines a reduire la riponse destructive aux stimuli Y Propulsion and Energetics Panel Chairman: Prof. Dr A.U$er Deputy Chairman: Mr R.E. Henderson Middle East Technical University Deputy for Technology ODTU Aero Propulsion & Power Laborawry Makina Miih. Boliimu WL/POT .. Ankara Wright Patterson Air Force Base Turkey OHIO 45433-6.563 United States PROGRAMME COMMITTEE Dr R.L.Derr, Chairman Professor D. Dini Head, Research Department Dipartimento di Macchine Code 38