Academic literature on the topic 'Missili cruise'

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Journal articles on the topic "Missili cruise"

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Bychkov, V. V. "Bychkov V. V. Strategic concept for the development of non-strategic missiles - sea-based complexes." National Security and Strategic Planning 2020, no. 4 (2021): 20–28. http://dx.doi.org/10.37468/2307-1400-2021-2020-4-20-28.

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The creation of a specific missile system with sea-based cruise missiles is determined by the principles of construction, solved goals and tasks. The priority areas for the development of promising missile weapons are factors such as: a combination of small weight and size character-istics of the missile and its area of an effective reflecting surface; optimization of flight altitude at cruise and final sections, at homing of cruise missiles on target; provision of antiosenitic ma-neuver and high speeds of cruise missiles flight to trajectories and much more.
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Yu, Yong Tao, and Ying Ding. "Application of Improved ANT Algorithm to Planning of Anti-Ship Cruise Missile Route." Advanced Materials Research 989-994 (July 2014): 1747–50. http://dx.doi.org/10.4028/www.scientific.net/amr.989-994.1747.

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Anti-ship cruise missile (ASCM) attack route meets the needs of the attack mission will determine the effect of the subsequent attacks. According to research planning of anti-ship cruise missile route based on improved ANT algorithm by elitist strategy. The first is sensitive factor analysis of route planning based on operational requirements. Second is established an objective function and constraints set of route planning, achieved anti-ship cruise missile route planning model. Finally, based on specific objectives, situation and the user's strategies, it can use improved ANT algorithm to pl
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Wade, Brian M. "A multi-objective optimization of ballistic and cruise missile fire plans based on damage calculations from missile impacts on an airfield defended by an air defense artillery network." Journal of Defense Modeling and Simulation: Applications, Methodology, Technology 16, no. 2 (2018): 103–17. http://dx.doi.org/10.1177/1548512918788503.

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This paper presents a new methodology for optimizing missile fire plan parameters in order to maximize the damage caused to an airfield by the impacts of ballistic and cruise missiles that leak through an air defense artillery network using weaponeering calculations. This new methodology models the damage to the airfield runway, fuel infrastructure, and parked aircraft caused by both unitary and submunition warheads carried by the ballistic and cruise missiles. It then uses the airfield damage models paired with an air defense simulation in a multi-objective optimization to find the non-domina
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Pereira, Carolina Almeida, Joana Moreira Ferreira, Francini Monteiro Costa, and Cristiana Guedes Oliveira. "A importância do LinkedIn nas estratégias de assessoria em turismo: estudo de caso de oito marcas de cruzeiros turísticos." Prisma.com 43 (2020): 130–57. http://dx.doi.org/10.21747/16463153/43a7.

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This work aims to understand the role that press office have and relate it with the importance of the social network, LinkedIn in press office tourism strategies. As such, a study case that involves eight brands related to cruises has been developed: Celebrity Cruises, Royal Caribbean International, Norwegian Cruise Line, Carnival Cruises, Princess Cruises, Holland America Line, MSC Cruises e Costa Cruises. In this way, we want to understand the impact that communication has on social media, especially on LinkedIn and on his mission. With this study, we conclude that LinkedIn is used as a plat
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Fuzhen, Shi, Guo Jinrui, and Ren Mingze. "Optimization Design of the Wing of Cruise Missile on the Basis of the Vortex Lattice Approach." Journal of Physics: Conference Series 2457, no. 1 (2023): 012034. http://dx.doi.org/10.1088/1742-6596/2457/1/012034.

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Abstract Aerodynamic performance of missile wings is a vital factor affecting the endurance and combat effectiveness of cruise missiles. Given the current situation that the aerodynamic design of conventional cruise missile wings is less and there is more room for improvement, a missile wing shape with a winglet is considered designed to improve the cruise characteristics of cruise missiles effectively. Firstly, the EPPLER 66 is selected as the wing shape by the combination of vortex surface element approach batch calculation and CFD simulation analysis. According to the dimensional parameters
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Munchak, Volodymyr, Oleksandr Vysikan, Oleksii Stepaniuk, and Yurii Maznychenko. "TO THE STUDY OF STRATEGIC CRUISE MISSILES X-101." Criminalistics and Forensics, no. 68 (July 3, 2023): 715–30. http://dx.doi.org/10.33994/kndise.2023.68.70.

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According to existing provisions, the examination of missile weapons is a set of expert research activities aimed at studying missile and jet weapons, as well as their components (mechanisms, assemblies, etc.) and their interaction in order to obtain reliable information about the objects provided for research. The article discusses some aspects of the research of missile weapons – strategic cruise missiles X-101, the relevance of which is due to their constant use in russia. Now russia is again carrying out massive missile strikes against Ukraine with X-101/55 missiles. The occupiers have cha
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Miskolczi, Márk, and Melinda Jászberényi. "Szállodahajó-turizmus a Dunán – trendek és termékfejlesztési lehetőségek Cruise tourism on the Danube – trends and product development opportunities." Turizmus Bulletin 21, no. 1 (2021): 13–25. http://dx.doi.org/10.14267/turbull.2021v21n1.2.

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Napjaink gyorsan változó fogyasztói trendjei folyamatos megújulásra ösztönzik a turizmuságazat szereplőit. A dunai szállodahajó-turizmus a szabadidős célú turisztikai utazások feltörekvő részterülete, ugyanakkor a hosszú távon is kiemelkedő gazdasági teljesítmény fenntartásához szükség van a termékkonstrukció időszakos megújítására. Jelen tanulmány a dunai szállodahajóturizmus alapismérveit, piaci (keresleti-kínálati) jellemzőit foglalja össze a témakörben publikált folyóiratcikkek elemzésén keresztül. Bemutatja továbbá a piacvezető vállalatok (Tauck, Avalon Waterways, Crystal Cruises, Uniworl
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Sriram Killi and Graham Injeti. "Feasibility of Integrating Cryogenic Propulsion for Next Generation Missiles for Enhanced Range, Stealth and Strategic Capabilities." Acceleron Aerospace Journal 3, no. 7 (2024): 764–84. https://doi.org/10.61359/11.2106-2475.

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The use of cryogenic propellants in missile propulsion systems has traditionally been limited due to the complexities associated with their storage and handling. However, cryogenic propellants, such as liquid hydrogen, offer significant advantages in terms of specific impulse and efficiency, making them a promising option for enhancing the range and performance of modern cruise missiles. Unlike traditional solid propellants, cryogenic fuels provide a higher specific impulse, which translates into better thrust efficiency and a more favorable stage mass ratio. This allows for longer flight dura
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Ding, Kun, Xuan Cui, Zhimei Wang, Zepeng Qiu, Yubao Hu, and Haiyan Zhang. "Research on Interception Model of Surface-to-air Missile Anti-cruise Missile Weapon System." Journal of Physics: Conference Series 2890, no. 1 (2024): 012006. http://dx.doi.org/10.1088/1742-6596/2890/1/012006.

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Abstract In air defense operations, resisting cruise missile attacks is a major challenge. Firstly, based on judging the direction and route of the cruise missile weapon system, the paper establishes the radar detection zone algorithm, the killing zone of surface-to-air missile weapon system and the interception model of surface-to-air missile weapon system needed in the process of physical interception. Secondly, according to whether the effective interception condition is satisfied, an algorithm is established to judge the surface-to-air missile weapon system on several fixed positions. Last
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Kovalev, M. A., and A. N. Nikitin. "Choosing the aerodynamic configuration of a subsonic cruise missile." VESTNIK of Samara University. Aerospace and Mechanical Engineering 18, no. 3 (2019): 59–66. http://dx.doi.org/10.18287/2541-7533-2019-18-3-59-66.

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The paper presents a comparison of two aerodynamic configurations of subsonic cruise missiles, characterized by the use of swept-back and forward-swept wings. The results of wind tunnel tests with the use of an automated measurement system characterizing the dependence of the lift and drag coefficients in a sufficiently wide range of angles of attack are presented. This allows us to compare the aerodynamic quality of the cruise missile models under investigation. The analysis of the results of experiments with the models and calculations in conditions of steady-state low-altitude horizontal fl
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Dissertations / Theses on the topic "Missili cruise"

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Bircan, Gokhan. "Cruise Missile Mission Rehearsal." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613948/index.pdf.

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Cruise missile mission planning is a key activity of cruise missile operations. Ground planning activities aim at low observable missions that have high probability of success. These activities include end game planning, route planning and launch planning. While end game planning tries to optimize end game parameters for maximum effectiveness, route planning tries to maximize survivability and enable navigational supports by determining the waypoints to from launch zone to target through a defended area. And lastly, planner tries to find the appropriate launch parameters that will prohibit pla
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Sparks, Timothy F. "The dawn of cruise missile diplomacy." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1997. http://handle.dtic.mil/100.2/ADA333251.

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Thesis (M.A. in National Security Affairs) Naval Postgraduate School, June 1997.<br>Thesis advisors, Peter R. Lavoy, Cynthia J. Levy. Includes bibliographical references (p. 61-64). Also Available online.
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Gauthier, Kathryn L. "AIRBORNE TELEMETRY AND CRUISE MISSILE CONTROL." International Foundation for Telemetering, 1985. http://hdl.handle.net/10150/615744.

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International Telemetering Conference Proceedings / October 28-31, 1985 / Riviera Hotel, Las Vegas, Nevada<br>The Advanced Range Instrumentation Aircraft (ARIA) is an airborne platform designed to receive, record, process, and retransmit telemetry data. This paper will provide a brief overview of ARIA capabilities and focus on a specially modified ARIA – the Cruise Missile Mission Control Aircraft (CMMCA). Currently utilized in cruise missile testing, CMMCA features on-board real-time display of telemetry data as well as remote command and control of the test missile.
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Kuykendall, Scott D. "Optimizing selection of Tomahawk Cruise Missiles." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA344719.

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Thesis (M.S. in Operations Research) Naval Postgraduate School, March 1998.<br>"March 1998." Thesis advisor(s): Richard E. Rosenthal. Includes bibliographical references (p. 39). Also available online.
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Le, Voyer Damien. "Guidance and Control of a Naval Cruise Missile." Thesis, KTH, Reglerteknik, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-105890.

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Today the armed forces of many countries need to strike accurately potential enemies, wherever they might be, from a safe place. Since naval units can be deployed almost everywhere in the open sea, the idea of a naval cruise missile emerged in the 70’s. These missiles are designed to be launched from various naval vehicles such as frigates or submarines and strike deeply in the enemy territory. A program called Missile de Croisière Naval (MdCN Naval Cruise Missile) was therefore launched in 2006 by the DGA, the French procurement agency. MBDA is the industrial company appointed by the DGA to d
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Dowling, William M. Soria Javier C. "Optimizing Ground Based Air Defense in support of homeland defense the cruise missile threat /." Monterey, Calif. : Naval Postgraduate School, 2006. http://bosun.nps.edu/uhtbin/hyperion.exe/06Dec%5FDowling.pdf.

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Thesis (M.S. in Defense Analysis)--Naval Postgraduate School, December 2006.<br>Thesis Advisor(s): Frank Giordano. "December 2006." Includes bibliographical references (p. 71-73). Also available in print.
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Ekutekin, Vedat. "Navigation And Control Studies On Cruise Missiles." Phd thesis, METU, 2007. http://etd.lib.metu.edu.tr/upload/12608142/index.pdf.

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A cruise missile is a guided missile that uses a lifting wing and a jet propulsion system to allow sustained flight. Cruise missiles are, in essence, unmanned aircraft and they are generally designed to carry a large conventional or nuclear warhead many hundreds of miles with excellent accuracy. In this study, navigation and control studies on cruise missiles are performed. Due to the variety and complexity of the subsystems of the cruise missiles, the main concern is limited with the navigation system. Navigation system determines the position, velocity, attitude and time solutions of the mis
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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, wi
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Camacho, Juan G., Lawrence F. Guest, Belen M. Hernandez, et al. "Open architecture as an enabler for FORCEnet Cruise Missile Defense." Thesis, Monterey, California. Naval Postgraduate School, 2007. http://hdl.handle.net/10945/6930.

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Advancements in missile technology have made cruise missile capability available worldwide. Current US naval weapon systems lack full interoperability across multiple platforms and full integration of detection, control, and engagement processes against incoming targets. The key to defeating future threats to our military assets is in gaining additional reaction time. This can be accomplished by leveraging collective sensor detection data throughout the battlespace, utilizing the FORCEnet data resources to evaluate the threat, and engaging the threat with a tiered defense. The objective of thi
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Jones, Antonio T. "Long-range precision-strike cruise missiles inNATO operations." Thesis, Monterey, California: Naval Postgraduate School, 2014. http://hdl.handle.net/10945/41399.

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Approved for public release; distribution is unlimited.<br>In 1949, NATO was established as a military alliance organized to protect its members from aggression or coercion by its adversaries to the East. However, after the collapse of the Soviet Union, the geostrategic context for NATO transformed significantly, with a new set of security threats (ethnic conflicts, terrorism, nuclear proliferation, organized crime, etc.). For NATO to remain relevant, its members had to sustain its overall purpose of collective defense and contribute to collective security in the post-Cold War world, in which
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Books on the topic "Missili cruise"

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Centre for Air Power Studies (New Delhi, India), ed. Cruise missiles: Evolution, proliferation, and future. KW Publishers in association with Centre for Air Power Studies, 2011.

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Canadian Institute for International Peace and Security., ed. The Cruise missile and cruise missile testing in Canada. Canadian Institute for International Peace and Security, 1988.

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Curren, Thomas. Cruise missiles. Library of Parliament, Research Branch, 1989.

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Larson, Eric V. Technological risk: The case of the Tomahawk cruise missile. Rand, 1990.

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Lempert, Robert J. Cruise missile arms control. Rand Corp., 1989.

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International Institute for Strategic Studies., ed. Dealing with the threat of cruise missiles. Oxford University Press, 2001.

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Gottemoeller, Rose E. Land-attack cruise missiles. International Institute for Strategic Studies, 1987.

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Werrell, Kenneth P. The evolution of the cruise missile. Air University, Air University Press, 1997.

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Werrell, Kenneth P. The evolution of the cruise missile. Air University, Air University Press, 1985.

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Carek, David A. Structural analysis of high-rpm composite propfan blades for a cruise missle wind tunnel model. National Aeronautics and Space Administration, 1993.

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Book chapters on the topic "Missili cruise"

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Naresh Kumar, G., Shweta Dadarya, Akshay Verandani, A. K. Sarkar, and S. E. Talole. "Cruise Missile Mission Planning Using Genetic Algorithm." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-5849-3_34.

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Ghoshal, Debalina. "Technological Aspects of Missile: Missiles and Warheads." In Role Of Ballistic And Cruise Missiles In International Security. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_2.

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Wittlinger, Sandra, and Alexis Papathanassis. "‘Missing in (Cruise-) Action’: Exploring Missing Passenger Incidents on Board Cruise Ships." In Tourism, Hospitality & Event Management. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-94664-1_2.

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Gottemoeller, Rose. "Verifying Controls on Cruise Missiles." In Verification and Compliance. Palgrave Macmillan UK, 1988. http://dx.doi.org/10.1007/978-1-349-10143-6_2.

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Thomas, Valerie. "Verification of Sea-Launched Cruise Missiles." In Verification of Arms Reductions. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-46684-7_5.

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Ghoshal, Debalina. "Why States Desire for Missile Systems?" In Role Of Ballistic And Cruise Missiles In International Security. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_4.

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Tsipis, Kosta. "Nuclear Cruise Missiles: The Problem of Verification." In The Arms Race in an Era of Negotiations. Palgrave Macmillan UK, 1991. http://dx.doi.org/10.1007/978-1-349-11967-7_7.

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Ghoshal, Debalina. "Survivability of Nuclear Missile Forces and Contemporary Debates." In Role Of Ballistic And Cruise Missiles In International Security. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-48063-8_6.

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Nalewajek, Robert A. "The Realities of Arms Control: The Cruise Missile Case." In Arms Control and Technological Innovation. Routledge, 2024. http://dx.doi.org/10.4324/9781003511717-14.

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Jobanputra, Ami, Dhruv Panchal, Het Trivedi, Dhyey Buch, and Bhavin Kakani. "Development of Antennas Subsystem for Indian Airborne Cruise Missile." In Proceedings of the International Conference on Paradigms of Computing, Communication and Data Sciences. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-7533-4_49.

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Conference papers on the topic "Missili cruise"

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Massey, Colin, Tiago Violante, and Lisa Highams. "One Engine Inoperative Cruise for Mission Performance Optimisation." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12847.

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Interest is growing in the use of one engine inoperative cruise to enhance the mission performance of multi-engined helicopters. This paper explores the concept by examining the use of twin engine cruise in the long range AgustaWestland AW101 triple engine helicopter. The paper presents the design features of the aircraft that support this capability, the clearances and limitations that have been flowed out to operators of the aircraft, analysis of the performance benefit arising from twin engine cruise, and examples of where the capability has been used to allow extreme range search and rescu
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Mao, Ruitong, Chengwei Yang, Yiyao Sun, et al. "Cruise Missile Weapon System Logic Architecture Design and Simulation Based on MBSE." In 2024 IEEE International Conference on Unmanned Systems (ICUS). IEEE, 2024. https://doi.org/10.1109/icus61736.2024.10840146.

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Liu, Mu, Guang Yue, Pei-Zhong Wang, and Lin Ren. "The Simulation Design of Attitude Control of Cruise Missile Based on Fireworks Algorithm." In 2024 International Conference on Cyber-Physical Social Intelligence (ICCSI). IEEE, 2024. https://doi.org/10.1109/iccsi62669.2024.10799324.

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Yang, Yizhen, Peng Lin, and Sentao Wu. "An Equalelevation Flight Method for Cruise Missiles based on Fuzzy Control." In 2024 43rd Chinese Control Conference (CCC). IEEE, 2024. http://dx.doi.org/10.23919/ccc63176.2024.10662423.

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D., Robert. "System Level Benefits of a Variable Diameter Rotor System for a Conceptual Tiltrotor Design." In Vertical Flight Society 74th Annual Forum & Technology Display. The Vertical Flight Society, 2018. http://dx.doi.org/10.4050/f-0074-2018-12726.

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This work presents a conceptual variable diameter tiltrotor sized in the NDARC conceptual design code. Both the maximum allowable diameter change and the weight increment due to morphing were varied with the intent of investigating the system level benefits (improved weight, fuel use, etc.) associated with a variable diameter rotor system. Generally, for a 0% increment in rotor weight due to morphing, diameter morphing reduced vehicle gross and component weights, as well as mission fuel weight. As the rotor weight penalty for morphing was increased, the entire system saw a corresponding increa
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"Cruise Missile." In Planet Austria. Verlag der Österreichischen Akademie der Wissenschaften, 2009. http://dx.doi.org/10.1553/planetaustrias164.

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Romanov, V. I., O. G. Zhiritsky, A. V. Kovalenko, and V. V. Lupandin. "M21 Cruise Marine Combined Cycle Plant." In ASME 1995 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1995. http://dx.doi.org/10.1115/95-gt-450.

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The paper describes M21 cruise marine combined cycle plant for SLAVA class cruisers (COGAG arrangement). Three guided missile cruisers (Figure 1) are powered by these plants (two plants for each cruiser). During this plant development the more strict demands on weight and size had been taken into account as compared with M25 plants for merchant ships. The paper shows technical data of M21 combined cycle plant, descriptions and design features of SPA MASHPROEKT GT 6004R gas turbine with reversible free power turbine, waste-heat recovery boiler, steam turbine with a condenser and a common gear u
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Edefur, Henrik, Fredrik Haglind, and Stefan Olsson. "Design of an Air-Launched Tactical Missile for Three Different Propulsion Systems: ATR, Rocket and Turbojet." In ASME Turbo Expo 2007: Power for Land, Sea, and Air. ASMEDC, 2007. http://dx.doi.org/10.1115/gt2007-27844.

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The objective of this paper is to assess the feasibility of a solid propellant Air Turbo Rocket (ATR), in comparison with a conventional turbojet engine or a solid rocket motor, as power source for a medium range tactical air-launched missile from an overall system point of view. A sizing method for missiles is developed, which together with flight performance calculations and engine performance data determines the final size and weight of the missile and its engine. The results suggest that an ATR engine is more favourable than a jet engine when the ratio between maximum (manoeuvre) thrust an
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Seigler, T. Michael, Jae-Sung Bae, and Daniel J. Inman. "Flight Control of a Variable Span Cruise Missile." In ASME 2004 International Mechanical Engineering Congress and Exposition. ASMEDC, 2004. http://dx.doi.org/10.1115/imece2004-61961.

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In this work the benefits of variable span morphing are considered, specifically with regards to the increased maneuverability of bank-to-turn cruise missiles. Along with an increase in range associated with variable span aircraft-in the case where both wings are equally extended-there is also the possibility of an additional advantage of higher control authority over both pitch and roll motions. In the case of roll control, one wing is extended while the other is contracted thus producing a moment about the longitudinal axis of the missile. Compared to conventional tail surface control, this
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Waldemark, Joakim T. A., Vlatko Becanovic, Thomas Lindblad, Clark S. Lindsey, Karina E. Waldemark, and Jason M. Kinser. "Pulse-coupled neural networks for cruise missile guidance and mission planning." In Ninth Workshop on Virtual Intelligence/Dynamic Neural Networks: Neural Networks Fuzzy Systems, Evolutionary Systems and Virtual Re, edited by Thomas Lindblad, Mary Lou Padgett, and Jason M. Kinser. SPIE, 1999. http://dx.doi.org/10.1117/12.343034.

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Reports on the topic "Missili cruise"

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Brockmann, Kolja, and Dmitry Stefanovich. Hypersonic Boost-Glide Systems and Hypersonic Cruise Missiles: Challenges for the Missile Technology Control Regime. Stockholm International Peace Research Institute, 2022. http://dx.doi.org/10.55163/bdyx5243.

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An increasing number of states are pursuing hypersonic missile development programmes, including for hypersonic boost-glide systems and hypersonic cruise missiles. Hypersonic missiles combine hypersonic speed and manoeuvrability which can result in target ambiguity, render missile defences ineffective and reduce warning times. Some hypersonic missiles are developed as delivery systems both for nuclear and conventional payloads. The combination of these capabilities may have escalatory or destabilizing effects. The Missile Technology Control Regime (MTCR) is the main instrument through which st
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Dunbar, William G., and Sidney W. Silverman. Cruise Missile Power System. Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada174324.

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Tissue, Phil, Ron Perkins, Darren Sawyer, and Lyle Powell. Attacking the Cruise Missile Threat. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada421607.

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Werrell, Kenneth P. The Evolution of the Cruise Missile. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada162646.

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Maloney, Michael S. Cruise Missile Attack Are We Prepared. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada469582.

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Woodside, Robert E., John McIver, Daniel Gadler, James Beyar, and James Howe. Feasibility of Third World Advanced Ballistic and Cruise Missile Threat. Volume 2: Emerging Cruise Missile Threat. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada377356.

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Sivakumaran, N. S., Paul A. Bigelman, Laura T. Lee, and Robert J. Jesionowski. The Probability of Negation of a Cruise Missile,. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada357518.

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Noone, Emily, and Lydia Harriss. Hypersonic missiles. Parliamentary Office of Science and Technology, 2023. http://dx.doi.org/10.58248/pn696.

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Abstract:
This POSTnote looks at hypersonic missile technologies, efforts to develop them, potential applications, and the possible challenges they may present for missile defence and global stability. Key Points: • Hypersonic missiles combine speeds of over five times the speed of sound with significant manoeuvrability during flight. • Their manoeuvrability enables them to change trajectory during flight, making their flight-path and target difficult to predict. • They fly at lower altitudes than ballistic missiles, which means that they may be harder to track at long distances with some surface-based
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Dale, C. J. Naval Arms Control: The Sea Launched Cruise Missile Debate. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada437745.

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Crupper, Jr, McDonald Charles G., and Richard T. The Ground-Launched Cruise Missile in NATO: Political Aspects. Defense Technical Information Center, 1988. http://dx.doi.org/10.21236/ada192610.

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