Hypersonic vehicles are exposed to severe heating loads during their flight in the atmosphere. In order to minimize the heating problem, a variety of cooling techniques are presently available for hypersonic blunt bodies. Introduction of a forward-facing cavity in the nose tip of a blunt body configuration of hypersonic vehicle is one of the most simple and attractive methods of reducing the convective heating rates on such a vehicle. In addition to aerodynamic heating, the overall drag force experienced by vehicles flying at hypersonic speeds is predominate due to formation of strong shock waves in the flow. Hence, the effective management of heat transfer rate and aerodynamic drag is a primary element to the success of any hypersonic vehicle design. So, precise information on both aerodynamic forces and heat transfer rates are essential in deciding the performance of the vehicle. In order to address the issue of both forces and heat transfer rates, right kind of measurement techniques must be incorporated in the ground-based testing facilities for such type of body configurations. Impulse facilities are the only devices that can simulate high altitude flight conditions. Uncertainties in test flow conditions of impulse facilities are some of the critical issues that essentially affect the final experimental results. Hence, more reliable and carefully designed experimental techniques/methodologies are needed in impulse facilities for generating experimental data, especially at hypersonic Mach numbers. In view of the above, an experimental program has been initiated to develop novel techniques of measuring both the aerodynamic forces and surface heat transfer rates. In the present investigation, both aerodynamic forces and surface heat transfer rates are measured over the test models at hypersonic Mach numbers in IISc hypersonic shock tunnel HST-2, having an effective test time of 800 s. The aerodynamic coefficients are measured with a miniature type accelerometer based balance system where as platinum thin film sensors are used to measure the convective heat transfer rates over the surface of the test model. An internally mountable accelerometer based balance system (three and six-component) is used for the measurement of aerodynamic forces and moment coefficients acting on the different test models (i.e., blunt cone with after body, blunt cone with after body and frustum, blunt cone with after body-frustum-triangular fins and sharp cone with after body-frustum-triangular fins), flying at free stream Mach numbers of 5.75 and 8 in hypersonic shock tunnel. The main principle of this design is that the model along with the internally mounted accelerometer balance system are supported by rubber bushes and there-by ensuring unrestrained free floating conditions of the model in the test section during the flow duration. In order to get a better performance from the accelerometer balance system, the location of accelerometers plays a vital role during the initial design of the balance. Hence, axi-symmetric finite element modeling (FEM) of the integrated model-balance system for the missile shaped model has been carried out at 0° angle of attack in a flow Mach number of 8. The drag force of a model was determined using commercial package of MSC/NASTRAN and MSC/PATRAN. For test flow duration of 800 s, the neoprene type rubber with Young’s modulus of 3 MPa and material combinations (aluminum and stainless steel material used as the model and balance) were chosen. The simulated drag acceleration (finite element) from the drag accelerometer is compared with recorded acceleration-time history from the accelerometer during the shock tunnel testing. The agreement between the acceleration-time history from finite-element simulation and measured response from the accelerometer is very good within the test flow domain. In order to verify the performance of the balance, tests were carried out on similar standard AGARD model configurations (blunt cone with cylinder and blunt cone with cylinder-frustum) and the results indicated that the measured values match very well with the AGARD model data and theoretically estimated values. Modified Newtonian theory is used to calculate the aerodynamic force coefficient analytically for various angles of attack. Convective surface heat transfer rate measurements are carried out by using vacuum sputtered platinum thin film sensors deposited on ceramic substrate (Macor) inserts which in turn are embedded on the metallic missile shaped body. Investigations are carried out on a model with and without fin configurations in HST-2 at flow Mach number of 5.75 and 8 with a stagnation enthalpy of 2 MJ/kg for zero degree angle of attack. The measured heating rates for the missile shaped body (i.e., with fin configuration) are lower than the predicted stagnation heating rates (Fay-Riddell expression) and the maximum difference is about 8%. These differences may be due to the theoretical values of velocity gradient used in the empirical relation. The experimentally measured values are expressed in terms of normalized heat transfer rates, Stanton numbers and correlated Stanton numbers, compared with the numerically estimated results. From the results, it is inferred that the location of maximum heating occurs at stagnation point which corresponds to zero velocity gradient. The heat-transfer ratio (q1/Qo)remains same in the stagnation zone of the model when the Mach number is increased from 5.75 to 8. At the corners of the blunt cone, the heat transfer rate doesn’t increase (or) fluctuate and the effects are negligible at two different Mach numbers (5.75 and 8). On the basis of equivalent total enthalpy, the heat-transfer rate with fin configuration (i.e., at junction of cylinder and fins) is slightly higher than that of the missile model without fin. Attempts have also been made to evaluate the feasibility of using forward facing cavity as probable technique to reduce the heat transfer rate and to study its effect on aerodynamic coefficients on a 41° apex angle missile shaped body, in hypersonic shock tunnel at a free stream Mach number of 8. The forward-facing circular cavities with two different diameters of 6 and 12 mm are chosen for the present investigations. Experiments are carried out at zero degree angle of attack for heat transfer measurements. About 10-25 % reduction in heat transfer rates is observed with cavity at gauge locations close to stagnation region, whereas the reduction in surface heat transfer rate is between 10-15 % for all other gauge locations (which is slightly downstream of the cavity) compared with the model without cavity. In order to understand the influence of forward facing cavities on force coefficients, measurement of aerodynamic forces and moment coefficients are also carried out on a missile shaped body at angles of attack. The same six component balance is also being used for subsequent investigation of force measurement on a missile shaped body with forward facing cavity. Overall drag reductions of up to 5 % is obtained for a cavity of 6 mm diameter, where as, for the 12 mm cavity an increase in aerodynamic drag is observed (up to about 10%). The addition of cavity resulted in a slight increase in the missile L/D ratio and did not significantly affect the missile lateral components. In summary, the designed balances are found to be suitable for force measurements on different test models in flows of duration less than a millisecond. In order to compliment the experimental results, axi-symmetric, Navier-Stokes CFD computations for the above-defined models are carried out for various angles of attack using a commercial package CFX-Ansys 5.7. The experimental free stream conditions obtained from the shock tunnel are used for the boundary conditions in the CFD simulation. The fundamental aerodynamic coefficients and heat transfer rates of experimental results are shown to be in good agreement with the predicted CFD. In order to have a feeling of the shock structure over test models, flow visualization experiments have been carried out by using the Schlieren technique at flow Mach numbers of 5.75 and 8. The visualized shock wave pattern around the test model consists of a strong bow shock which is spherical in shape and symmetrical over the forebody of the cone. Experimentally measured shock stand-off distance compare well with the computed value as well as the theoretically estimated value using Van Dyke’s theory. These flow visualization experiments have given a factual proof to the quality of flow in the tunnel test section.

North Korea twice conducted ballistic missile tests close to Japan in 1998 and 2006. While Japan responded with non-coercive condemnations to demonstrate its disapproval in 1998, it imposed unilateral economic sanctions in 2006, marking the first instance in post-World War II of applying a substantial coercion to punish a neighbouring state. The research asks why Japanese policy toward the North shifted for a seemingly identical type of provocation. The dissertation seeks contextual explanations by using inductive process-tracing, a type of ‘middle approach’ between historical narratives and parsimonious theories. It is applied to highlight the underlying mechanism through which public discursive changes concerning national security and North Korea during this eight-year period influenced the subsequent policy shift in 2006. The dissertation concludes that the unilateral sanctions were not necessarily a calculated strategic response to punish the missile launch (or North Korean nuclear programs) per se, but were a direct consequence of a deeper shift in societal discourse taking place beforehand. During the eight-year period, there had been other visible provocations and shocks originating from the North, especially the sensational revelation in 2002 of past North Korean abductions of Japanese citizens. These highly-publicized incidents facilitated the Japanese public to be increasingly conscious about Japan’s security weaknesses and re-evaluate its historical relations with its neighbour, leading to a hardened domestic environment in which the new idea of pressuring the North became a feasible option even before 2006. These North Korean provocations and the resulting societal security discourse, along with concurrent structural changes in the Japanese government and mass media which made them both highly susceptible to discursive currents among citizens, mutually interacted to produce the policy result when the opportunity arose. The research, however, also challenges the popular view that the sanctions are the first example of the wholesale transformation of Japan’s post-war ‘pacifist’ security principles. It argues that the confined means (economic) by which the sanctions were imposed reflects the highly nuanced discourse, which endorses Japan’s legitimate right to specifically punish the North for the harms done, but that the societal momentum is not equally supportive of the more controversial areas concerning military usage and the current constitution.

North Korea twice conducted ballistic missile tests close to Japan in 1998 and 2006. While Japan responded with non-coercive condemnations to demonstrate its disapproval in 1998, it imposed unilateral economic sanctions in 2006, marking the first instance in post-World War II of applying a substantial coercion to punish a neighbouring state. The research asks why Japanese policy toward the North shifted for a seemingly identical type of provocation. The dissertation seeks contextual explanations by using inductive process-tracing, a type of ‘middle approach’ between historical narratives and parsimonious theories. It is applied to highlight the underlying mechanism through which public discursive changes concerning national security and North Korea during this eight-year period influenced the subsequent policy shift in 2006. The dissertation concludes that the unilateral sanctions were not necessarily a calculated strategic response to punish the missile launch (or North Korean nuclear programs) per se, but were a direct consequence of a deeper shift in societal discourse taking place beforehand. During the eight-year period, there had been other visible provocations and shocks originating from the North, especially the sensational revelation in 2002 of past North Korean abductions of Japanese citizens. These highly-publicized incidents facilitated the Japanese public to be increasingly conscious about Japan’s security weaknesses and re-evaluate its historical relations with its neighbour, leading to a hardened domestic environment in which the new idea of pressuring the North became a feasible option even before 2006. These North Korean provocations and the resulting societal security discourse, along with concurrent structural changes in the Japanese government and mass media which made them both highly susceptible to discursive currents among citizens, mutually interacted to produce the policy result when the opportunity arose. The research, however, also challenges the popular view that the sanctions are the first example of the wholesale transformation of Japan’s post-war ‘pacifist’ security principles. It argues that the confined means (economic) by which the sanctions were imposed reflects the highly nuanced discourse, which endorses Japan’s legitimate right to specifically punish the North for the harms done, but that the societal momentum is not equally supportive of the more controversial areas concerning military usage and the current constitution.

This is a historic structure report for the C-47 Nike missile launch site in Wheeler, Indiana. This report provides a description, condition assessment, and recommendation for restoration of the site since it has sustained damage from weather, fire, and vandals. The site is listed on the State Register and National Register of Historic Places and the Nike Preservation Group desires to turn the site into a Cold War museum and memorial.A history of the Cold War and development of the Nike missile systems and C-47 site provides the background of the project. Each structure and feature is described and the condition recorded. Recommendations for treatment and maintenance are provided. Suggestions are made for a phased restoration of the site to accommodate a Cold War museum. Since it is recommended the site be open to the public, issues regarding public health, safety, security, and handicap accessibility are addressed. This project does not provide a full management and preservation plan, measured HABS/HAER drawings, or a structural analysis. / Department of Architecture

The official reaction of the Russian Federation and of the People's Republic of China to the announcement made by the United States in December 2001 to abrogate the almost thirty years old Anti-Ballistic Missile (ABM) Treaty has been remarkably weak, given their sustained and coordinated opposition to the deployment of strategic defences against ballistic missiles (BMD). Because the existing literature, particularly balance of power theory, under-explored this puzzle and fails to provide a satisfactory explanation to it, a neoclassical realist model building on structural and unit-level variables is proposed to supplement this caveat. It is argued that Russia, as a stagnant great power experiencing trouble at the domestic level, bandwagons with the United States because it discounts the medium- and long-term threat posed by BMD. China, a rising developmental state, is soft balancing because it resents the project and the threat it poses to its security. It has not hard balanced so far because there is an acknowledgement that this could jeopardize its power base, as the telling example of the USSR collapse illustrated.

Studiens syfte är att öka förståelsen för möjligheterna med modern artificiell intelligens (AI) vid militär användning genom att bidra med information om ny teknik. Moderna civila applikationer av datorseende som skapats genom användande av så kallade artificiella neurala nät visar resultat som närmar sig den mänskliga synens nivå när det gäller att känna igen olika saker i sin omgivning. Denna studie motiveras av dessa observationer inom området AI i förhållande till situationer i luftstrid då pilotens syn används för att känna igen flygplan innan det bekämpas. Exempelvis vid användande av hjälmsikte riktar pilotens ögon målsökaren hos en luftmålsrobot mot det flygplan som robotens målsökare sedan låser på. Utanför visuella avstånd kan pilotens ögon av naturliga skäl inte användas på detta sätt, varför datorseende använt i en luftmålsrobot undersöks. Resultaten från studien stödjer att datorseende genom användande av artificiella neurala nät kan användas i en luftmålsrobot samt att datorseende kan utföra uppgiften att känna igen stridsflygplan. / This study is aimed at increasing the knowledge to those concerned within the Armed Forces by providing information on the possibilities of modern artificial intelligence (AI). Motivation comes from observations of civilian technology on the use of AI in the field of Computer Vision showing performance equaling the level of the human vision when using the technology of Deep Learning of Artificial Neural Nets. In air-combat aircraft the pilot´s vision is used for recognizing the aircraft that is about to be shot down. For example when utilizing helmet mounted displays, the seeker of an air-target-missile is directed upon the aircraft on which the pilot´s eyes are looking. However when air-target-missiles are utilized beyond visual range the pilot´s vision cannot help in directing the seeker on a specific target. Therefore computer vision within an air-target-missile is studied. The results of the study support that the technology of neural networks may be used in an air-target-missile and that computer vision provided by this technology can do the job of recognizing a combat aircraft.

Com a Revolução Cubana a Guerra Fria se torna mais presente no continente americano. O governo dos Estados Unidos da América começa a desenvolver ações para combater o governo revolucionário que assume o poder naquele país. Essas ações são baseadas no emprego da força militar e em soluções diplomáticas. Nesse mesmo período, João Goulart se torna presidente do Brasil. Ele continua a Política Externa Independente do governo Jânio Quadros. E o governo brasileiro acaba se envolvendo na questão de Cuba. Esta tese procura investigar a participação do governo de João Goulart na Crise dos Mísseis (1962) e compreender o que esse episódio representa para a Política Externa Independente. Nossos objetivos são demonstrar como o Brasil percebe a evolução da questão de Cuba; perceber como o país se posicionou na Organização dos Estados Americanos (OEA) e quais foram as repercussões decorrentes; procurar entender qual a razão do envio do general Albino Silva à Cuba; compreender a posição brasileira na Organização das Nações Unidas (ONU) através do projeto de desnuclearização da América Latina; verificar como a sociedade brasileira se manifestou a respeito desse episódio; e, por fim, analisar se a Crise dos Mísseis modifica as relações entre os governos de Goulart e Kennedy. / With the Cuban Revolution to Cold War becomes more present in the Americas. The government of the United States of America begins to develop actions to combat the revolutionary government that assumes power in that country. These actions are based on the use of military force and diplomatic solutions. In the same period, becomes president of Brazil João Goulart. He continues the Política Externa Independente of Quadros government. And the brazilian government gets involved in the issue of Cuba. This thesis investigates the involvement of the government of João Goulart in Missile Crisis (1962) and understand what this episode is for the Política Externa Independente. Our objectives are to demonstrate how Brazil sees the evolution of the issue of Cuba; see how the country stood at the Organization of American States (OAS) and what were this repercussions; seek to understand the reason of sending general Albino Silva the Cuba; understand the brazilian position at the United Nations (UN) through the project of denuclearization of Latin America; check how brazilian society manifested related to this episode; finally, analyze the Missile Crisis produced some effect in relations between the governments of Goulart and John Kennedy; analyze if the Missile Crisis modifies the relations between the government of Goulart and Kennedy.

In this thesis, the problem of intercepting highly manoeuvrable threats using seeker-less interceptors that operate in the command guidance mode, is addressed. These systems are more prone to estimation errors than standard seeker-based systems. Several non-linear and optimal estimation and guidance concepts are presented in this thesis for interception of randomly maneuvering targets by seeker-less interceptors. The key contributions of the thesis can be broadly categorized into six groups, namely (i) an optimal selection of bank of lters in interactive multiple model (IMM) scheme to cater to various maneuvers that are expected during the end-game, (ii) an innovative algorithm to reduce chattering phenomenon and formulate effective guidance algorithm based on 'differential game guidance law' (modi ed DGL), (iii) IMM/DGL and IMM/modified DGL based integrated estimation/guidance (IEG) strategy, (iv) sensitivity and robustness analysis of Kalman lters and ne tuning of lters in filter bank using innovation covariance, (v) Performance of tuned IMM/PN, tuned IMM/DGL and tuned IMM/modi ed DGL against various target maneuvers, (vi) Performance comparison with realistic missile model. An innovative generalized state estimation formulation has been proposed in this the-sis for accurately estimating the states of incoming high speed randomly maneuvering targets. The IMM scheme and an optimal selection of lters, to cater to various maneu-vers that are expected during the end-game, is described in detail. The key advantage of this formulation is that it is generic and can capture evasive target maneuver as well as straight moving targets in a uni ed framework without any change of target model and tuning parameters. In this thesis, a game optimal guidance law is described in detail for 2D and 3D engagements. The performance of the differential game based guidance law (DGL) is compared with conventional Proportional Navigation (PN) guidance law, especially for 3D interception scenarios. An innovative chatter removal algorithm is introduced by modifying the differential game based guidance law (modified DGL). In this algorithm, chattering is reduced to the maximum extent possible by introducing a boundary layer around the switching surface and using a continuous control within the boundary layer. The thesis presents performance of the modified DGL algorithm against PN and DGL, through a comparison of miss distances and achieved accelerations. Simulation results are also presented for varying fiight path angle errors. Apart from the guidance logic, two novel ideas have been presented following the evolving "integrated estimation and guidance" philosophy. In the rst approach, an in-tegrated estimation/guidance (IEG) algorithm that integrates IMM estimator with DGL law (IMM/DGL), is proposed for seeker-less interception. In this interception scenario, the target performs an evasive bang-bang maneuver, while the sensor has noisy measure-ments and the interceptor is subject to an acceleration bound. The guidance parameters (i.e., the lateral acceleration commands) are computed with the help of zero e ort miss distance. The thesis presents the performance of the IEG algorithm against combined IMM with PN (IMM/PN), through a comparison of miss distances. In the second ap-proach, a novel modi ed IEG algorithm composed of IMM estimator and modi ed DGL guidance law is introduced to eliminate the chattering phenomenon. Results from both of these integrated approaches are quite promising. Monte Carlo simulation results re-veal that modi ed IEG algorithm achieves better homing performance, even if the target maneuver model is unknown to the estimator. These results and their analysis o er an insight to the interception process and the proposed algorithms. The selection of lter tuning parameters puts forward a major challenge for scien-tists and engineers. Two recently developed metrics, based on innovation covariance, are incorporated for determining the filter tuning parameters. For predicting the proper combination of the lter tuning parameters, the metrics are evaluated for a 3D interception problem. A detailed sensitivity and robustness analysis is carried out for each type of Kalman lters. Optimal and tuned Kalman lters are selected in the IMM con guration to cater to various maneuvers that are expected during the end-game. In the interception scenario examined in this thesis, the target performs various types of maneuvers, while the sensor has noisy measurements and the interceptor is subject to acceleration bound. The tuned IMM serves as a basis for synthesis of e cient lters for tracking maneuvering targets and reducing estimation errors. A numerical study is provided which demonstrates the performance and viability of tuned IMM/modi ed DGL based modi ed IEG strategy. In this thesis, comparison is also performed between tuned IMM/PN, tuned IMM/DGL and tuned IMM/modi ed DGL in integrated estimation/guidance scheme. The results are illustrated by an extensive Monte Carlo simulation study in the presence of estimation errors. Simulation results are also presented for end game maneuvers and varying light path angle errors . Numerical simulations to study the aerodynamic e ects on integrated estimation/ guidance structure and its e ect on performance of guidance laws are presented. A detailed comparison is also performed between tuned IMM/PN, tuned IMM/DGL and tuned IMM/modi ed DGL in integrated estimation/guidance scheme with realistically modelled missile against various target maneuvers. Though the time taken to intercept is higher when a realistic model is considered, the integrated estimation/guidance law still performs better. The miss distance is observed to be similar to the one obtained by considering simpli ed kinematic models.

Com a Revolução Cubana a Guerra Fria se torna mais presente no continente americano. O governo dos Estados Unidos da América começa a desenvolver ações para combater o governo revolucionário que assume o poder naquele país. Essas ações são baseadas no emprego da força militar e em soluções diplomáticas. Nesse mesmo período, João Goulart se torna presidente do Brasil. Ele continua a Política Externa Independente do governo Jânio Quadros. E o governo brasileiro acaba se envolvendo na questão de Cuba. Esta tese procura investigar a participação do governo de João Goulart na Crise dos Mísseis (1962) e compreender o que esse episódio representa para a Política Externa Independente. Nossos objetivos são demonstrar como o Brasil percebe a evolução da questão de Cuba; perceber como o país se posicionou na Organização dos Estados Americanos (OEA) e quais foram as repercussões decorrentes; procurar entender qual a razão do envio do general Albino Silva à Cuba; compreender a posição brasileira na Organização das Nações Unidas (ONU) através do projeto de desnuclearização da América Latina; verificar como a sociedade brasileira se manifestou a respeito desse episódio; e, por fim, analisar se a Crise dos Mísseis modifica as relações entre os governos de Goulart e Kennedy. / With the Cuban Revolution to Cold War becomes more present in the Americas. The government of the United States of America begins to develop actions to combat the revolutionary government that assumes power in that country. These actions are based on the use of military force and diplomatic solutions. In the same period, becomes president of Brazil João Goulart. He continues the Política Externa Independente of Quadros government. And the brazilian government gets involved in the issue of Cuba. This thesis investigates the involvement of the government of João Goulart in Missile Crisis (1962) and understand what this episode is for the Política Externa Independente. Our objectives are to demonstrate how Brazil sees the evolution of the issue of Cuba; see how the country stood at the Organization of American States (OAS) and what were this repercussions; seek to understand the reason of sending general Albino Silva the Cuba; understand the brazilian position at the United Nations (UN) through the project of denuclearization of Latin America; check how brazilian society manifested related to this episode; finally, analyze the Missile Crisis produced some effect in relations between the governments of Goulart and John Kennedy; analyze if the Missile Crisis modifies the relations between the government of Goulart and Kennedy.

The purpose of this thesis is to explain why states obtain nuclear weapons and the role various actors and interests play in the making of states´ nuclear policies. The main questions are as follows: (1) What big theories exist concerning states obtaining nuclear weapon and nuclear armament in International Relations and what relevance do they have of the post cold-war period?, (2) What is the meaning of the perspective of the Military-Industrial Complex (MIC)?, and (3)Are there empirical studies which supports the existence of a MIC in the United States? The focus lies on actors and driving forces that are internal to states and it is also important to investigate if the theories have relevance for the post 9/11-era. The study uses the method of qualitative literature-study with some quantitative segments. It is claimed that states might be interested in justifying their behaviour in a morally appealing way and that real reasons may be hidden. There are many reasons for states to obtain and keep nuclear weapons and related technology (which includes many of the most lucrative elements of the arms industry´s sales). Among this reasons are that arms and related technology may be used to influence other states and nuclear weapons-construction and modernisation might be used to protect the state from external threats, stop unwanted interference from other actors, secure job and gain recognition and prestige in world politics. For security reasons states might hold onto their own nuclear weapons and try to hinder other actors from getting access to them. The internal actors and driving forces we look at are bureaucratic, economical and political, and the MIC-perspective. The military can be said to have interests in as much resources and capabilities as possible, which includes advanced weaponary such as nuclear weapons and related technologies, at its disposal because of the goal to defend the state from all possible threats and for officers career reasons. Much of its influence is said to come from its expert knowledge and position and it is said to be especially influential in matters of foreign policy, military spending and foreign policy. The major economical actors mentioned are big corporations involved in military spending and these have interests in maximizing profits. Nuclear weapons making and maintenance and the related areas of missile defense and delivering methods for nuclear weapons seem to be areas with high changes of being profitable for the involved major companies. The actors wield influence for example through lobbying and campaign contributions. An economic driving force claim is that state spending is necessary for stimulating the economy and defense spending is easily justified in other ways. Political actors and driving forces concerns politicians interest in promoting the interests of supporting groups, there are indications that the weapon industry is such a group. Research have shown various results about the extent politicians tend to further the interests of supporting groups. The MIC-perspective talks about groups with interest in high levels of military spending. Most researchers seem to agree that the complex exists but there are different opinions about what actors belongs to it and its power on various issues. There is some mention of the core of the complex consisting of such internal actors as mentioned above. MIC-related empirical research has been conducted and this author finds that the MIC is a relevant analytical tool for the post cold war – and 9/11 era.