The mx missile and multiple protective structure basing. Aerodynes use the concept of pushing the air or gas downwards so that due to newtons law of motion to generate an upward force to push the aircraft upwards. Structural design and fabrication of a rocket michael r. It is assumed that the object decelerates in one hundredth of a second 0. The assumption of a rigid structure is necessary in the prelim inary design phase of a missile in order to allow the computation of loads on which further design. Amcp 706286, structures, forming part of the ballistic missile series of the army materiel command engineering design handbook series, is published for the information and guidance of all concerned. Design and analysis of surface to surface missile srikanth bashetty 1, likhitha chodisetti 2 1assistant professor, department of aeronautical engineering, mlr institute of technology, jntu hyderabad, telangana, india, 2b. Abstract a missile is a selfpropelled precisionguided munition system, as opposed to an unguided self. Bechtel, design of structures for missile impact, topical.
Calculation of airphase load and airframe design of a typical missile. Analysis and design of missile structures 1967 edition. This phenomenon corresponds to a fluid airstructure interaction leading to high amplitudes of low frequency vibrations. Introduction it can determine whether our design of a control system meets the specification if the desired time response of the controlled variable determined. Pdf in order to improve the quality and efficiency of missile design, it would be better to take structure design into account during the prophase of. Analysis and design of missile structures in searchworks catalog. Missile design and system engineering aiaa education series. Rapid structure design and automated adjustment of missile body. Defense technical information center compilation part notice. From the above contours, at the converging points pressure and temperature increases and decreases at the diverging points. So, what exactly happened on this mediumrange airtoair missile is that structural degradations occurred during the captive flight of a combat aircraft in specific phases of the flight, known as buffeting. Geographic information systems and geographic data mining services and software are available. V depends on the ratio m s m p one way to increase range is to add propellant. The modular design of the missile and its capability of being launched at different orientations enable it to be integrated with a wide spectrum of platforms like warships, submarines, different types of aircraft, mobile.
Case design is usually governed by a combination of motor and vehicle requirements. In a few cases it may be possible to structure design, carriage environment, modify modsify, a aut launch lnc platform plstcato to toi accommodate a modate an oonew a newstuur geometryweight dein constraints caige of the aircraft, nvomn,aircraft missile, but in most cases this is not an option. Mar 29, 2019 the lambda missile design is computationally analyzed in ansys fluent to get more accurate results. In order to reduce the manual workload and improve the efficiency of research and development, a general integrated method of missile structure modeling, analysis and. While in the design phase, this must be taken into account. Accelerating binary genetic algorithm driven missile design. In a few cases it may be possible to structure design, carriage environment, modify modsify, a aut launch lnc platform plstcato to toi accommodate a modate an oonew a newstuur geometryweight dein constraints caige of the aircraft, nvomn,aircraft.
We conclude that the design criteria and procedures described by this report are acceptable to the regulatory staff and that bctop9, revision 2, is acceptable by reference in applications for construction permits and operating licenses. Pdf rapid structure design and automated adjustment of missile. The lambda missile design is computationally analyzed in ansys fluent to get more accurate results. Variable structure based nonlinear missile guidance and autopilot design for a direct hit with thrust vector control.
In this study, a general integrated method for design, analysis and optimization of missile structure has been proposed for the rapid conceptual design of missile structure, by which the relatively optimal result can be obtained efficiently. Pmf where p impact force f acceleration retardation. Stanford libraries official online search tool for books, media, journals, databases, government documents and more. Technologies of missile ballistic components for the design of the missile was used the design and modelling program catia v5 r21, in which was made an design of the component piece of the missile model, based on the existent missile model. Structural design of missiles and spacecraft caltech magazine. In this study, nonlinear modeling and dynamical analysis of a surface to air missile. Structural analysis and design optimization of a missile. The structure team was allocated approximately 1500 dollars. The next design parameter that has to consider is the weight of the rocket. The objective of the publication is to communicate the work performed at the laboratory to its sponsors and to the scientific and engineering communities, defense establishment, academia, and industry. Aimed toward the needs of aerospace engineering students and professors, system analysts and engineers, program managers, and others working in the areas of missile system and missile technology development, the book provides readers with an understanding of missile design, missile technologies, launch platform integration, missile system. Design, ballistic missile, propulsion system, manufacturing technologies. That makes the missile heavier and the forces greater.
The johns hopkins apl technical digest is an unclassified technical journal published quarterly by the applied physics laboratory. The results presented are validation metrics, performance metrics of simulator studies and optimization studies, and future. Additionally, various missile examples are provided to verify the effectiveness of this method. Proceedings of the 41st ieee conference on decision and control, 2002. Light to carry and easy to operate, the fim92 stinger is a passive surfacetoair missile that can be shoulderfired by a single operator although standard military procedure calls for two operators, team chief and gunner. Besides constituting the structural body of the rocket motor with its nozzle, propellant grain, and so on, the case frequently serves also as the primary structure of the missile or launch vehicle.
This 75 page pdf titled usaf ballistic missile fiscal years 1964 to 1966 is one of the best documents available that explores the history of the design and development of the minuteman weapon system and the numerous challenges faced as the minuteman became the primary air force contribution to the strategic missile force. During the early design phase, computer analyses using. Missile design and systems engineering is a substantial update with significant new material, including an integration of systems engineering considerations with the missile design process. Structural components general dynamics ordnance and.
Design of missile guidance law via variable structure control. Simulating flow of mach 4 over the missile at angle of attack of 0 q, 45 q and 60 q and plotting pressure variation, velocity variation, density variati on and temperature variation. Th design is imported and covered with the fluid domain of 2 m distance from the missile as shown in the next figure. Pdf calculation of airphase load and airframe design of a. April 20 name typesystem length m diameter mcep payload kg range km accuracy propulsion guidance status agm86c 1 alcm 6. The results of the missile tests indicated that some partially grouted brick veneer cavity walls could also be used as the exterior shelter walls. In military language, a missile, also known as a guided missile, is a guided airborne ranged weapon capable of selfpropelled flight usually by a jet engine or rocket motor. The shuttle achieved firstflight readiness through a series of localized structural modifications and operational flight constraints. Standard missile 3 iia is a ballistic missile interceptor. Supersonic cruise missile travels at a speed of around 23 mach i. Japanese cooperative design that will be deployable on land as at sea, defend broader areas with a larger kinetic warhead.
Dec 15, 2009 analysis and design of missile structures by e. The design and development of satellite launch vehicle and missile are driven by the need for minimum weight structures. The multicell design not only permits a reduction in overall missile length. A rapid missile body structure design module was developed based on nx environment and method above which can achieve rapid structure design, automated adjustment, as well as automated calculation. For most of missile configurations, this interest required thrust vector control together with conventional aerodynamic control. Designing the outer struc ture of surface to surface missile in catia v5r20 and obtaining a 3d model. Longterm budgetary implications the congress of the united states congressional budget office for sale by the superintendent of documents, u. Based on the demand of improving the efficiency in missile body structure design, we studied the parametric description, layout design and modeling method of missile body structures and developed a missile body structure rapid design module on nx, realising the rapid design and automated adjustment of missile body structures as well as the. Design guidelines related to use of dynamic capacity increase factors, allowable ductility ratio and allowable range of steel ratios used in concrete structural. However, formatting rules can vary widely between applications and fields of interest or study. The sensor could be a satellite, radar or airborne ir system 2 sensor cues the early warning sensor performs one to three hits on the threat missile to determine its characteristics and direction 3 defence interceptor assigned through a preplanned command structure and battlefield.
Ebook download pdf missile design and system engineering aiaa education, by eugene l. In the demonstration phase of a missile scheme, to obtain the optimum proposal, designers need to modify the parameters of the overall structure frequently and significantly, and perform the structural analysis repeatedly. Missile and space structures composite rocket motors and launch tubes for tactical and strategic missiles launched from ground, air, ship and submarine platforms. Some parts used must be purchased commercially due to the complexity of them, however others must be manufactured in house by the structure team. Use lighter than air gases such as hot air, hydrogen, helium. For years, i have used his tactical missile design as the goto reference for missile design activities. Lincoln operations provides the composite interstage which provides structure for the missile. Bruhn, 1967, tristateoffset co edition, in english. Structural design of missiles and spacecraft staff, 1962 structural design of missiles and spacecraft. The orbiter structure was designed to an early set of loads and conditions and certified to a later set. This phenomenon corresponds to a fluid air structure interaction leading to high amplitudes of low frequency vibrations.
If you scale both the propellant and structure up by the same factor, you dont gain any velocity. Pdf rapid structure design and automated adjustment of. Abstract a missile is a selfpropelled precisionguided. Structure magazine tornado debris impact testing and masonry. Missile load for wdc3 frame equivalent static methodology 6 the missile shield is designed for tornado generated missile impact loads for wdc3 structure as shown below. In order to improve the quality and efficiency of missile design, it would be better to take structure design into account during the prophase of missile preliminary design instead of later phase. Particujar attention has been given to the stress analysis of thin shells. Your feedback will be important as we plan further development of our repository. Pdf on jan 14, 2016, osama kamal mahmoud and others published analysis and material design of missiles structures find, read and cite all the research you need on researchgate. Tec h scholar, department of aeronautical engineering, mlr institute of technology, jntu hyderabad, telangana, india. Composite drive shafts and tubes filamentwound composite drive shafts and tubular products for both aerospace and commercial applications.
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