Relevant bibliographies by topics / Guided missiles Guided missiles Air-to-surface missiles

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Academic literature on the topic 'Guided missiles Guided missiles Air-to-surface missiles'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Guided missiles Guided missiles Air-to-surface missiles"

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Fino, Steven A. "Doubling Down." Vulcan 2, no. 1 (June 23, 2014): 125–61. http://dx.doi.org/10.1163/22134603-00201005.

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The us Air Force’s and Navy’s semi-autonomous radar- and infrared-guided air-to-air missiles performed miserably in air combat over Vietnam. Despite accusations that the military’s overreliance on complex technology was to blame, the two services continued to invest in ever-more advanced fighter aircraft and high-tech missiles after the war. In 1977 at the behest of Congress, the Air Force and Navy spent almost a full year evaluating air combat tactics and new infrared-guided air-to-air missiles. According to the services’ interpretation of the results from the aimval and aceval tests, future air combat demanded both improved infrared-guided missiles and revolutionary radar-guided missiles. The apparent paradox—testing infrared missiles to justify a more expensive radar-guided missile—was seized on by the military “Reformers” as emblematic of the us military’s unhealthy fascination with exorbitantly priced high-technology. This paper discusses the pivotal aimval-aceval tests, including their laborious design process and execution, and their subsequent role animating the early-1980s public debate over military technology. This understanding is crucial when evaluating the relative significance of organizational inertia in the Air Force’s air-to-air procurement decisions following Vietnam. Additionally, the aimval-aceval tests offer evidence of three pathologies that distinguish military tests from their typical civilian exemplars: military tests cannot be conducted independent of the service(s); the tests are generally inflexible and unreplicable; and their data are usually shrouded by classification concerns. These pathologies make it difficult to reconcile divergent interpretations and resolve controversies that emerge from military testing activities.
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Faqih, Kamil, Sujito Sujito, Siti Sendari, and Faiz Syaikhoni Aziz. "Smart guided missile using accelerometer and gyroscope based on backpropagation neural network method for optimal control output feedback." Journal of Mechatronics, Electrical Power, and Vehicular Technology 11, no. 2 (December 22, 2020): 55. http://dx.doi.org/10.14203/j.mev.2020.v11.55-63.

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As a maritime country with a large area, besides the need to defend itself with the military, it also needs to protect itself with aerospace technology that can be controlled automatically. This research aims to develop an air defense system that can control guided missiles automatically with high accuracy. The right method can provide a high level of accuracy in controlling missiles to the targeted object. With the backpropagation neural network method for optimal control output feedback, it can process information data from the radar to control missile’s movement with a high degree of accuracy. The controller uses optimal control output feedback, which is equipped with a lock system and utilizes an accelerometer that can detect the slope of the missile and a gyroscope that can detect the slope between the target direction of the missile to follow the target, control the position, and direction of the missile. The target speed of movement can be easily identified and followed by the missile through the lock system. Sampling data comes from signals generated by radars located in defense areas and from missiles. Each part’s data processing speed is calculated using a fast algorithm that is reliable and has a level of accuracy and fast processing. Data processing impacts on the accuracy of missile movements on any change in the position and motion of targets and target speed. Improved maneuvering accuracy in the first training system can detect 1000 files with a load of 273, while in the last training, the system can detect 1000 files without a load period. So the missile can be guided to hit the target without obstacles when maneuvering.
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Xie, Wei Shi, Zhi Hua Xiao, and Jian Tang. "The Design Research of Millimeter-Wave Homing Empty - Empty Ammunition Ballistics." Applied Mechanics and Materials 575 (June 2014): 337–42. http://dx.doi.org/10.4028/www.scientific.net/amm.575.337.

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The millimeter-wave terminal guidance ammunition monitoring scanning field is small. The modified design is in order to improve the search section trajectory guidance. This study established seeker search area to capture the target model, which leads to the missile engine unpowered glide distance formula after flameout. At the millimeter-wave terminal on the missiles contraction section ballistic. Each missile is designed for the flat road, the swash decline ballistic programs. Flat missile road program scans and does not shrink. Its flight speed falls and declines rapidly, has different gliding distance and terminal velocity. After the missile engine is flameout, its start-gliding speed is great. Ramp fell ballistic program enhances the air-air (or air-ground) guided missile’s gliding ability, helping to improve range. But shortcomings are that target tracking scanning domain contracts. Using the seeker optical axis in the pitch direction can achieve accurate positioning with the height precession. Two ballistic designs can both meet the target seeker’s scanning, thus effectively improve the striking precision.
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Thong, Do Quang. "Synthesis of High-Precision Missile Homing System Using Proportional Guidance Method." Mekhatronika, Avtomatizatsiya, Upravlenie 21, no. 4 (April 11, 2020): 242–48. http://dx.doi.org/10.17587/mau.21.242-248.

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Modern air targets are characterized by low visibility, high maneuverability and high survivability. In addition, for some specific targets, for instance ballistic missiles, in order to defeat them the missile need tobe guided and carried out direct hit, i.e. "hit to kill". Therefore, in this paper, we present a high-precision missile homing system (MHS) using the proportional guidance method for firing at the highly maneuverable targets. Specifically, we propose a parametric optimization method for choosing a set of optimal parameters of the missile homing system for each dynamic parameter set of the missile. In addition, the paper gives the recommendations of choosing the initial conditions for the synthesis of missile homing system. In our experience, we should choose the small initial condition for synthesizing the missile homing system. Finally, the article also investigates the influence of systematic error in determining the speed, normal acceleration of missiles and the angular velocity of the line of sight of the missile and target on the accuracy of the missile homing system. We implement the proposed missile homing system and the parametric optimization method in Matlab. The experimental results illustrate that, using proposed system and the parametric optimization method, the missile can defeat the modern air targets with low visibility, high maneuverability and high survivability.
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Shyshanov, M., O. Zubariev, O. Hurba, and Y. Kryzhanivskyi. "ASSESSING THE EFFECTIVENESS OF REPAIR GUIDED AVIATION MEANS OF DE-STRUCTION." Collection of scientific works of the Military Institute of Kyiv National Taras Shevchenko University, no. 64 (2019): 36–44. http://dx.doi.org/10.17721/2519-481x/2019/64-04.

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The article presents the general requirements for the level of reliability of guided aviation means of destruction (GAMD), which can be applied based on the requirements for performance indicators of operation. This depends on the set of tactical, technical and operational characteristics of GAMD, which determine their level technical excellence, as well as a method for assessing the effectiveness of guided aviation means of destruction, based on the progressive standard method. The estimation of the coefficient of technical excellence of samples of armaments, which reveal their level of development and is carried out in relation to their classification, has been considered. During the analysis, the most important performance characteristics are considered. They define the basic architecture and design of this type of armaments and have the greatest influence on their combat missions. The basics of their functioning and the order of their intended using are more fully considered in a number of sources. The developed method of comparative estimation of GAMD is intended for comparison of possible variants and allows to define complex indicators of quality that take into account most of all existing properties of GAMD, to assess its conformity to tactical and technical requirements, quantitative requirements and state standards. Moreover, it allows conducting a comparative assessment of domestic and foreign samples of armaments. The basic performance characteristics of short-range guided aviation missiles of the Air-to-Air class with infrared heads and their foreign analogues are given. The purpose of this article is to conduct a preliminary calculation of the level of technical excellence and analysis of the priority directions of development of air guided missiles of the Air-to-Air class.
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Sonawane, Hemant R., and Shripad P. Mahulikar. "Tactical air warfare: Generic model for aircraft susceptibility to infrared guided missiles." Aerospace Science and Technology 15, no. 4 (June 2011): 249–60. http://dx.doi.org/10.1016/j.ast.2010.07.008.

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Dobrzyński, Paweł, Stanisław Lipski, Bogdan Machowski, Rafał Miętkiewicz, and Tomasz Olszewski. "An automated module of self-defence and masking of naval vessels of the Polish Navy with the use of miniature rocket missiles caliber 70 and 40 mm." Zeszyty Naukowe Akademii Marynarki Wojennej 214, no. 3 (September 1, 2018): 137–60. http://dx.doi.org/10.2478/sjpna-2018-0023.

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Abstract This article is an attempt to interest the subjects associated with maritime technology — in the possibilities of increasing the safety of Polish Navy ships (or civilian ships), which may be threatened by attacks of maneuvering missiles and drones moving at low altitude at high speed. The concept proposed by the team was initially verified in simulation tests and the obtained results of these studies indicate that the automated missile self-defence system based on guided and unguided missiles with caliber 40 mm and 70 mm, can be an effective means of self-defence (even the smallest vessels). Small dimensions and mass as well as simplicity of use and reliability of this weapon system allow to believe that 40 mm MLRS1 could also be used by special forces of Polish Navy in offensive operations (destruction of lightly armoured objects of surface or ground, vehicles, force, putting smoke screens, mine mines) to 2000 m. For that reason, the system is referred to by the team of implementers as ‘pocket rocket artillery’.
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Baranik, O., V. Berezanskii, A. Datsenko, and О. Tesnikov. "APPLICATION OF THE PRINCIPLE OF RELATION TO CHOOSE THE TECHNICAL OPERATION PROGRAM OF GUIDED AIR WEAPONS AT TRANSITION TO OPERATION ACCORDING TO TECHNICAL CONDITION." Collection of scientific works of the National Academyof the National Guard of Ukraine 2, no. 36 (2020): 44–54. http://dx.doi.org/10.33405/2409-7470/2020/2/36/223552.

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The article presents the current state of the available stock of guided air weapons and the problem of transition of guided air weapons to operation according to technical condition. The transfer of guided air weapons to operation according to technical condition involves increasing the role of measurement operations and control of their parameters and characteristics. This will determine the actual technical condition and make informed decisions about further operation. In general, the effective-ness of control a technical condition of aviation missiles significantly affects the readiness for use of aviation equipment and the combat capabilities of this equipment in performance of the tasks. The exciting control model and methods for selecting parameters of technical condition is universal in relation to the variants of construction of the technical maintenance program a guided air weapons allows to conduct research into these indicators. However, this program does not indicate the plural of variant that should be selected if the undetermined influence of different nature factors to carry out a set of maintenance and repair work for guided air weapons. The possibility of using the principle of correlation, when choosing the program of technical operation a guid-ed air weapons during the transition to operation according to technical condition. With the help of the correlation principle, an approach to the choice of the program of technical operation a guided air weapons can be developed in case of unknown infor-mation about the mechanisms of influence of various internal and external factors on the properties of the guided air weapons, their effect on the technical condition and features of the units of aviation guided missile that are not amenable to instrumental con-trol. To implement the control of guided air weapons with using a principle of correlation need to use the results of practical appli-cations of aviation guided missile, including other types of fire tests, sample tests using the physico-chemical analysis of powder and explosive charges.
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Swietochowski, Norbert, and Dariusz Rewak. "‘KRAB’ – new capabilities of the Polish Armed Forces." Scientific Journal of the Military University of Land Forces 188, no. 2 (June 30, 2018): 141–61. http://dx.doi.org/10.5604/01.3001.0012.2501.

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The implementation of 155 mm self-propelled howitzers ‘Krab’ into the Missile and Artillery Forces significantly improve their capabilities. Apart the howitzer, the battalion fire module ‘Regina’ consists of specialized command, reconnaissance, support and ammunition vehicles. The caliber of the howitzer adjusted to NATO standards allows for the application of the common ammunition, including precision-guided, with the range up to 40 km, which will enable striking the important targets in the enemy’s rear combat zone. An artillery battalion (battery) equipped with the self-propelled howitzer ‘Krab’ owing to usage of the precision-guided munitions during the engagement will gain unprecedented capabilities with regards to impacting a target. Moreover, the battalion will be able to successfully fulfill tasks, which until recently could be executed by a general-military commander with the support of anti-tank reserves, tank subunits, special forces or tactical surface-to-surface missiles. The paper proposes organizational structures of the ‘Krab’ artillery battalion, variants of order of battle and methods of fire tasks execution.
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Kieley, Marc. "No umbrella for the rain: Canadian implications following the global revolution in reconnaissance–strike technologies." International Journal: Canada's Journal of Global Policy Analysis 76, no. 2 (June 2021): 221–37. http://dx.doi.org/10.1177/00207020211019301.

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Global conflicts in 2020 have highlighted the unexpected employment of advanced ballistic missiles and unmanned aerial vehicles by developing military powers. The development of ballistic missiles by Iran, or the export of advanced drones by Turkey, are ultimately the result of the American-led revolution in military affairs that, during the Gulf War, established the potential of precision guided weapons and reconnaissance systems. In response, America’s competitors have adapted their military doctrines and developed weapons designed to both counter and copy the West’s technological advantages. As the Government of Canada implements its defence policy—Strong, Secure, and Engaged—it has promised to procure a ground-based air defence system for the Canadian Armed Forces. Careful consideration and analysis are required, however, to ensure that Canada procures the best possible solution given limited funding and a wide array of potential threats.
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Dissertations / Theses on the topic "Guided missiles Guided missiles Air-to-surface missiles"

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Chichka, David F. "Cruise-dash optimization applied to an air-breathing missile." Thesis, Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/90923.

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The method of singular perturbations is applied to the determination of the optimal range-fuel-time trajectory for an air-breathing missile. This method is shown to lead to the reduced-order "cruise-dash" model, and this model is used in the optimization study. Earlier work in this area is extended by the inclusion of two not heretofore considered limits on the dynamical system. The results of the earlier work are shown to hold throughout much of the velocity regime in which the missile operates, but operation in the very high and very low velocity ranges is shown to be sharply curtailed, with the optimal operating points being changed drastically in some cases. Also, the effect of the non-zero minimum admissible throttle setting and the resultant throttle-chattering on the solution of the control problem is examined in some detail.
M.S.
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Kumar, Renjith R. "Optimal and near-optimal medium range air-to-air missile guidance against maneuvering targets." Diss., Virginia Polytechnic Institute and State University, 1989. http://hdl.handle.net/10919/54224.

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Optimal intercept trajectories for a boost-sustain-coast medium-range air-to-air missile are synthesized using optimal control theory. Optimality in time/range/energy at intercept of a target is the main objective. Attainable sets and their boundaries are obtained and used to generate optimal intercept points in a three-dimensional scenario. A three-phase closed-loop guidance scheme is used to generate an efficient guidance law against a maneuvering target. In the present study, target maneuvers are restricted to the horizontal plane. An initial boost-phase with near-optimal guidance in the presence of active control constraints and thrust switches is simulated. Target maneuvers are neglected during this phase. A new method of gain evaluation is detailed. A midcourse guidance scheme with neighboring guidance, transversal comparisons, and chasing center-of-attainability of target to augment performance is studied. Modifications in terminal guidance using proportional navigation, such as chasing the center-of-attainability of target, altitude shaping, and drag-resolution schemes are used to attempt better performance at intercept. A composite guidance strategy using a combination of neighboring guidance and proportional navigation for the midcourse guidance is introduced. The excellent performance of this guidance strategy and the improvement in storage requirements for on-board use make it a very special scheme.
Ph. D.
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Abell, Barry J. "Planning concepts to sustain, develop, and test complex naval combat systems at the Surface Combat Systems Center, Wallops Island, Virginia." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Mar%5FAbell.pdf.

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Thesis (M.S. in Systems Engineering Management)--Naval Postgraduate School, March 2005.
Thesis Advisor(s): Scott Carlson, Benjamin Roberts. Includes bibliographical references (p. 145-152) Also available online.
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Turco, Kyle T. "Development of the Joint Stand Off Weapon (JSOW) moving target capability AGM-154 Block Three program /." 2006. http://etd.utk.edu/2006/TurcoKyle.pdf.

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Books on the topic "Guided missiles Guided missiles Air-to-surface missiles"

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Institute of Defence Studies and Analyses., ed. Space age gladiators: Surface to surface missiles and air strategy : an Indian viewpoint. New Delhi: Knowledge World in association with Institute of Defence Studies and Analyses, 2000.

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Suyan, Wu, and Liu Yi, eds. Gao ji shu zhan zheng zhong de jing que da ji: Kong di zhi dao wu qi. Beijing: Jie fang jun wen yi chu ban she, 2002.

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Office, General Accounting. Precision-guided munitions: Acquisition plans for the joint air-to-surface standoff missile : report to congressional committees. Washington, D.C: The Office, 1996.

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Office, General Accounting. Precision-guided munitions: Acquisition plans for the joint air-to-surface standoff missile : report to congressional committees. Washington, D.C. (441 G St., NW, Room LM, Washington 20548): U.S. General Accounting Office, 1996.

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Office, General Accounting. Precision-guided munitions: Acquisition plans for the joint air-to-surface standoff missile : report to congressional committees. Washington, D.C. (441 G St., NW, Room LM, Washington 20548): U.S. General Accounting Office, 1996.

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Hamilton, Thomas. Expendable missiles vs. reusable platform costs and historical data. Santa Monica, CA: RAND, 2012.

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Shutty, Michael Allen. Dynamic modeling and modal analysis of an air-to-air missile. Monterey, California: Naval Postgraduate School, 1991.

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Office, General Accounting. Contract pricing: Overpricing of joint cruise missiles automatic test equipment : report to the Director, Cruise Missiles Project, Naval Air Systems Command. Washington, D.C: The Office, 1988, 1988.

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1956-, Paul Detlev, ed. V2 gefrorene Blitze: Einsatzgeschichte der V2 aus Eifel, Hunsrück und Westerwald 1944/45 : eine Dokumentation. 2nd ed. Aachen: Helios, 2007.

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Hollinger, Kristy. Nike Hercules operations in Alaska, 1959-1979. Alaska]: U.S. Army Garrison Alaska, 2004.

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Conference papers on the topic "Guided missiles Guided missiles Air-to-surface missiles"

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Barrett, Ron. "20 Years of Adaptive Aerostructures in Flying Missiles, Munitions and UAVs." In ASME 2014 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/smasis2014-7662.

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In September of 1994 a small uninhabited aerial vehicle took to the air. While the flight of this lightweight powered glider was unremarkable, its 3 minutes aloft represented a turning point in adaptive aerostructures technology as it was the first man-made craft to stay aloft while using only adaptive materials for all flight control. This paper celebrates and summarizes two decades of flying adaptive aerostructures controlling missiles, munitions and UAVs. The paper starts with an historical review of the technologies which underpinned the first adaptive flight vehicles. Twist-active piezoelectric plates are shown beside the earliest flightweight stabilators they were integrated into. A brief description of the 120cm wingspan UAV “Mothra” which took to the air 20 years ago is given. The earliest hard-launched adaptive actuators were designed and developed just a year after Mothra took to the air. The paper summarizes the resulting (unrestricted) adaptive actuator configurations which have come around since that time, including actuator assemblies for guided bullets and cannon shells from 5.56mm through 155mm. A decade ago, the first post-buckled precompressed (PBP) piezoelectric flight control mechanisms debuted as enabling technologies in a unique class of aircraft: “hovering missiles” flew at international airshows, guided rounds hit targets on gunnery ranges and entered serial production with PBP actuator assemblies. More modern incarnations of these actuators and others have been designed into GPS-guided grenade, mortar and artillery shells. Today, some of the world’s most active and highest work energy density actuators are built with ultra-high strain adaptive materials and have been shown to dramatically cut CEP of gravity weapons, cruise missiles and glide shells. The paper concludes with a chart showing which classes of adaptive actuators have been flown in what types of weapon systems and UAVs over the past 20 years.
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Schumacher, Lauren N., and Ronald M. Barrett. "Guided Munition Adaptive Trim Actuation System for Aerial Gunnery." In ASME 2018 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/smasis2018-8032.

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Twenty-two years ago, adaptive munitions using piezoelectric actuators were conceived. The Barrel-Launched Adaptive Munition (BLAM) program used piezoelectric elements to articulate a 10 deg. half-angle conical section on the nose of a 73 mm caliber supersonic wind tunnel model. The test article was designed to pivot the forward portion of the round about the aerodynamic center (which was collocated with the forward section center of gravity). While effective in trim articulation, the majority of actuator power was expended resisting nose inertia rather than manipulating air loads. Adaptive actuators for guided munitions have progressed greatly since that time. In 2001, major advances canard articulation for guided bullets were achieved. These were followed by the Shipborne Countermeasure Range-Extended Adaptive Munition (SCREAM) program. While the piezoelectric effectors designed for these historic programs would allow for respectable deflections, the invention of post-buckled piezoelectric (PBP) actuation would dramatically boost total deflection levels while maintaining full blocked force capabilities. These PBP actuators would be used in a variety of flight control mechanisms for different classes of UAVs. In addition to these applications, the high bandwidth of piezoelectric actuators are particularly well suited to guided munitions. This paper describes the structural mechanics and dynamics of the PBP-class actuator as integrated in guided munitions. As a critical element in ultra-high bandwidth flight control actuation, PBP actuators have been shown to possess pseudo-corner frequencies in excess of 1 kHz. Additionally, PBP actuators have been integrated into tight packing volumes in guided cannon shells while demonstrating setback acceleration tolerances of tens of thousands of g’s. Previous work illustrates several different actuation configurations as well as integration methods with canards and fins. This study links the structural mechanics of previous authors with aeromechanics to arrive at performance predictions in aerial combat. The paper lays out a guided aerial round based on the PBP concept, then uses circular error probable (CEP) predictions in a standard atmosphere quantify the required deflections for engagement of a variety of targets. The results show one order of magnitude fewer rounds being expended per kill in direct air-to-air engagements with peer aircraft. The paper shows that PBP-class actuators could be used for defensive engagements as well with the engagement of oncoming hostile missiles. The paper concludes with prediction of engagement improvements for modern aircraft like the F-35 with 25 mm rounds as well as aircraft like the F-15 with 20 mm guided ammunition.
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Saied, Ahmed Samier, A. N. Ouda, and Wagdy R. Anis. "Modeling and Simulation Synthesis for an Air-to-Air Guided Missile." In 2018 14th International Computer Engineering Conference (ICENCO). IEEE, 2018. http://dx.doi.org/10.1109/icenco.2018.8636129.

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Said, Ahmed Samir, and A. N. Ouda. "Design of a Robust Classical PI Controller for an Air-To-Air Guided Missile." In 2020 International Conference on Innovative Trends in Communication and Computer Engineering (ITCE). IEEE, 2020. http://dx.doi.org/10.1109/itce48509.2020.9047819.

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Zhaohui, Hu, Luo Jixun, and Yang Liu. "Research on Anti-jamming Performance Test Planning of Active Radar Guided Air-to-Air Missile." In 2014 7th International Symposium on Computational Intelligence and Design (ISCID). IEEE, 2014. http://dx.doi.org/10.1109/iscid.2014.10.

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Patterson, Jeffrey S., Donald J. Hoffman, and Linda M. Ochs. "Allison 501-K17 SSGTGS Technical Directive Experience." In ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-gt-169.

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The Allison 501-K17 Ship Service Gas Turbine Generator Set (SSGTGS) is used is provide ship board electrical power on several U.S. Navy Class ships, including the DD-963 Spruance Destroyer, the DDG-993 Kidd Guided Missile Destroyer and CG-47 Ticonderoga Guided Missile Cruiser Classes. The first of these units were placed in service during the mid 1970s. The Naval Sea Systems Command (NAVSEA) in conjunction with the Naval Surface Warfare Center, Carderock Division, Ship Systems Engineering Station (NSWCCD-SSES) have undertaken a major upgrade effort to improve the reliability, operation, serviceability and maintainability of the unit. This paper examines the process of this program and details the specific improvements made to the unit as a result of this effort. In addition, this paper outlines the experience gained as a result of installing these upgrades in the Fleet.
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Ehler, Andrew, Christopher Hoppe, Hayden Kovarik, Reed Lamy, Connor Loo, Aaron Moore, Benjamin Shu, and Matthew Snyder. "Design and Test of an Articulation Mechanism for a Morphing Missile Nosecone." In ASME 2020 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/smasis2020-2215.

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Abstract This paper covers the design and development of a mechanism to change the angle of an air-to-air missile nosecone relative to the missile body while in flight. A group of senior cadets at the United States Air Force Academy performed the work in fulfillment of requirements for their capstone design project. The Air Force Research Laboratory (AFRL) sponsored the project and provided a set of requirements to guide the design. These requirements include the challenge of torque transfer under significant loading in order to drive the nosecone to a new angle. The report will cover significant design changes from last year’s design and the justification for these changes. A complete sub-system breakdown follows. Finally, the planned testing and evaluation of the design is discussed.
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Tong, Michael T. "A Probabilistic Risk-Based Approach to Assess NASA Aeronautics Technologies." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-91007.

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NASA’s aeronautics research program invests in air-transportation technologies to protect the environment, makes air travel more accessible and affordable for Americans, enables exploration through new aerospace missions, and augments national security. The program will address critical public needs related to reduction of aircraft noise and emissions, and enable new science missions. In this paper, a probabilistic risk-based approach is presented to provide guidance for developing a robust technology portfolio, and to prioritize the most promising technologies required to achieve aeronautics program goals. An assessment of subsonic aircraft emission-reduction technologies is performed to demonstrate how the approach can be used to guide technology investment in the context of limited NASA funding for aeronautics technology research.
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Reinauer, G. A., and M. Peszynski. "Weight Reduction in a Marine Gas Turbine Inlet." In ASME 1985 International Gas Turbine Conference and Exhibit. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-gt-75.

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Major design changes to the Propulsion Gas Turbine Air Inlet on the US Navy’s CG47 Class Guided Missile Cruisers have resulted in significant superstructure weight savings. The majority of weight reduction resulted from use of finite element analysis (FEA) computer modeling techniques applied to structural optimization. FEA models of the forward and aft deckhouses provided the necessary capability to analyze each structure’s response to loads simulating a nuclear air blast, shock, and vibration. Integration of the moisture separator housings into each deckhouse structure allowed improved structural stability and additional weight reductions. FEA modeling and a redesign of the major inlet system 32% lighter than inlets installed onearly ships of this class. The first of the lightweight deckhouses has been installed on the CG52 Cruiser.
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Galel, Zev, James L. Hunt, and Thomas H. Unger. "Laser Guidance for Repairing Gas Turbine Parts." In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1994. http://dx.doi.org/10.1115/94-gt-006.

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As a result of normal operating conditions, jet engine parts tend to distort. During repair, many of these parts require some form of selective cutting. Due to the differences between each individual part, automation such as CNC machining becomes complex. The need to map each individual part prior to machining has prohibited repair facilities from introducing sophisticated automation. This paper presents for the first time a novel method that addresses many problems related to selective material removal in Jet Engine repairs. Similar to a terrain-following cruise missile, a laser guided cutter is used to follow a selected datum surface. For example, in the case of Honeycomb Airseals, the thin laser beam penetrates through the honeycomb cell structure to follow the base metal. The method minimizes parent metal removal and under-minimum-wall condition. As a result, life potential of parts is extended, and repair costs are reduced. The ability to track a moving part and modify the cutting path automatically produces one more significant advantage: accurate set-up of a part on a machine is no longer critical. The method has applications in the repair of airseals, frames and cases, and airfoils.
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Reports on the topic "Guided missiles Guided missiles Air-to-surface missiles"

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Ebbs, Raymond E. SAC (Strategic Air Command) Needs a Few Good Men and Women' - A Guide to ICBM (Intercontinental Ballistic Missile) Operations Duty. Fort Belvoir, VA: Defense Technical Information Center, April 1988. http://dx.doi.org/10.21236/ada197073.

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