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Relevant bibliographies by topics / Rocket

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Dissertations / Theses
Books
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Academic literature on the topic 'Rocket'

Author: Grafiati

Published: 4 June 2021

Last updated: 26 July 2025

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Journal articles on the topic "Rocket"

1

Anggara Trisna Nugraha, Alwy Muhammad Ravi, and Dadang Priyambodo. "Optimization of Targeting Rocket Launchers with Wheeled Robots." Journal of Electronics, Electromedical Engineering, and Medical Informatics 3, no. 1 (2021): 44–49. http://dx.doi.org/10.35882/jeeemi.v3i1.7.

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The quick launch weapon system is unique. This rocket launcher has a high launch rate, but the rocket launched is one stage lower than the launcher normally launched by ships of this size. For example, a (medium) cruiser would use a fast light rocket launcher to launch a light (small) rocket. Currently rocket launchers are still controlled by humans, using PCs and servo motors as control tools to determine the accuracy of the shooting angle, so complete components are needed when designing the robot so that the robot can work automatically as needed. For the input given, Automatically control

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Anggara Trisna Nugraha and Dadang Priyambodo. "Analysis of Determining Target Accuracy of Rocket Launchers on Xbee-Pro based Wheeled Robots to Realize the Development of Technology on the Military Field." Journal of Electronics, Electromedical Engineering, and Medical Informatics 2, no. 3 (2020): 114–18. http://dx.doi.org/10.35882/jeeemi.v2i3.5.

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At this time the rocket launcher is still controlled by humans who utilize technology using a PC and a servo motor as a control device to determine the accuracy at the shooting angle, in designing this robot complete components are needed so that the robot can work automatically according to the input given, the rocket launcher robot controlled automatically by communication from the PC after which the command is forwarded to the microcontroller using a USB TTL cable and sent to the Xbee-pro sender circuit then transmitted and received by the Xbee-pro receiver then transmitted to the microcont

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Amar, S., and Reddy T. Gowtham Manikanta. "Air Breathing Rocket Engines and Sustainable Launch Systems." Applied Mechanics and Materials 232 (November 2012): 310–15. http://dx.doi.org/10.4028/www.scientific.net/amm.232.310.

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An air-breathing rocket engine inhales oxygen from the air for about half the flight, so it doesn't have to store the gas onboard. So at take-off, an air-breathing rocket weighs much less than a conventional rocket, which carries all of its fuel and oxygen onboard. Air breathing rockets, combine the performance characteristics of both rocket and ramjet engines. An air-breathing engine gets its initial take-off power from specially designed rockets, called air-augmented rockets, that boost performance about 15 percent over conventional rockets. When the vehicle's velocity reaches twice the spee

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Křepský, Martin. "Rocket Engines’ Solid Propellants and Combustion Products." Science & Military 19, no. 2 (2024): 36–42. https://doi.org/10.52651/sam.a.2024.2.36-42.

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Rocket technology has shown considerable progress in recent decades. In addition to peaceful use, rockets are used in the military as a means of transporting destructive charges on a target. Any information obtained, even a partial one, could be used to prevent or mitigate a missile threat. Different types of rocket engines are sources of rocket propulsion. One of the factors by which individual types of rockets differ from each other is the type of fuel used. Combustion of rocket fuel creates a flame that is a source of radiation. The article analyzes the composition of different types of sol

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Lu, Zhishan. "Recent Advances of Design Optimization Techniques in Solid Rocket." Highlights in Science, Engineering and Technology 37 (March 18, 2023): 252–61. http://dx.doi.org/10.54097/hset.v37i.6080.

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A solid-propellant rocket or solid rocket refers to a rocket with an engine using solid propellants. The earliest solid rockets were powered by gunpowder. It is still used today in military armaments worldwide, model rockets, solid rocket boosters and on larger applications for their simplicity and reliability. With the fast development in the complexity of rockets, the importance of optimisation where the overall performance is maximised has been shown. Engineers are routinely given design tasks to find a design meeting the stringent constraints. For instance, researchers developed different

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Wang, Tao, Lin Ding, and Huahuang Yu. "Research and Development of Fault Diagnosis Methods for Liquid Rocket Engines." Aerospace 9, no. 9 (2022): 481. http://dx.doi.org/10.3390/aerospace9090481.

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Currently, considerable efforts are being focused on the development of reusable rockets and smart rockets due to the heavy requirements of future next-generation aerospace transportation. Safety, low-launching cost, and repeatability are expected from liquid rocket for fulfilling the big dreams of space transportation, exploration, and travelling. Therefore, research on fault detection of the liquid rocket engines (LRE) is critical for satisfying the above claims. Therefore, a comprehensive survey on the research and development of fault diagnosis systems and methods for the liquid rocket eng

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ZAGANESCU, Nicolae-Florin, Rodica ZAGANESCU, and Constantin-Marcian GHEORGHE. "Wernher Von Braun’s Pioneering Work in Modelling and Testing Liquid-Propellant Rockets." INCAS BULLETIN 14, no. 2 (2022): 153–61. http://dx.doi.org/10.13111/2066-8201.2022.14.2.13.

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This paper presents a view on how Dr. Wernher Von Braun laid the basis for realistic modelling and testing liquid-propellants rockets, by his PhD Thesis – a secret document in 1934, which remained classified until 1960. Understanding that better mathematical modelling is needed if these rockets are to become spaceflight vehicles, he clarified in his thesis essential issues like: maximum achievable rocket speed; Laval nozzle thrust gain; polytropic processes in the combustion chamber and nozzle; influence of equilibrium and dissociation reactions; original measurement systems for rockets test s

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Ye, Zhenru. "Analysis of the Mechanical Principle of Water Rocket Launch and Its Design." Academic Journal of Science and Technology 3, no. 2 (2022): 194–97. http://dx.doi.org/10.54097/ajst.v3i2.2172.

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Water rocket is a common physical extracurricular production work. In practice, the author has found that there are many improvements available. Based on the study of the mechanical principles of water rocket launch, the performance and safety of water rocket are improved through analysis and improvement of design. At the same time, the launch of rocket, the separation of first and second stage rockets, as well as recovery are observed from multiple angles using on-board cameras, thus achieving full simulation of rocket launch.

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An, Junming, and Bingji Li. "Application and Comparison of Additive Manufacturing Technology in Rocket Manufacturing." Highlights in Science, Engineering and Technology 76 (December 31, 2023): 296–307. http://dx.doi.org/10.54097/4r1k0e19.

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Engineering's most difficult and complex challenges have always been those involving the production of rockets. Rocket manufacturing has benefited greatly in recent years from the three-dimensional(3D) printing technology's quick development. By layering materials, 3D printing technology can produce complicated parts and components with accuracy and efficiency. However, there are certain distinctions in how various 3D printing methods are applied while making rockets. This article will introduce several common 3D printing technologies and their applications in the manufacturing of key rocket c

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Andi, Susilo, Yasmiati, and Apandi Ahmad. "Low cost NodeMcu based development water rocket measurement system applied to STEM education." TELKOMNIKA Telecommunication, Computing, Electronics and Control 17, no. 3 (2019): 1513–20. https://doi.org/10.12928/TELKOMNIKA.v17i3.12227.

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Water rockets have become one of learning tools for STEM Education in schools. Generally water rockets make in school activity have no parachute load, altitude, and velocity measurement. Rocket can go any direction and also will cause hard collision to the ground that break the high speed rocket. It will take time and need more cost to make a new one for students. This study propose the low cost NodeMcu based water rocket measurement system to solve the problem. Altitude and velocity measurement are added and deployment system to release the parachute to make water rocket fall to the ground sm

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Dissertations / Theses on the topic "Rocket"

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Fernandez, Margaret Mary. "Propellant tank pressurization modeling for a hybrid rocket /." Online version of thesis, 2009. http://hdl.handle.net/1850/10631.

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Abrahamsson, Paulina, Maja Johannesson, and Nellie Reichel. "Rocket Padel : Rocket Padels order-till-leveransprocess, från inhouse till outsourcing." Thesis, Linnéuniversitetet, Institutionen för ekonomistyrning och logistik (ELO), 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:lnu:diva-105973.

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Titel: Rocket Padel - Rocket Padels order-till-leveransprocess, från inhouse till outsourcing Författare: Paulina Abrahamsson, Maja Johannesson, Nellie Reichel Handledare: Petra Andersson Examinator: Hana Hulthén Bakgrund: Trenden kring outsourcing är något som pågår än idag och fortsatt visa sig lönsamt för företag. Rocket Padels nuvarande lager saknar den kapacitet som krävs för att kunna hantera de ökade antalet ordrar, som har tillkommit med dess tillväxt på marknaden. Utan tillräckligt med lagerkapacitet och resurser för att lyckas hantera den ökade antalet ordrar, kommer Rocket Padel

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Bell, Luke. "Rocket science : phytochemical, postharvest, shelf-life & sensory attributes of rocket species." Thesis, University of Reading, 2016. http://centaur.reading.ac.uk/69943/.

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Rocket species are increasing in popularity with consumers, and in the last ten years scientific interest has also increased due to the potential health benefits of consuming leaves. They are known for pungent and bitter taste components, and the chemical compounds largely responsible for these sensations are also health beneficial. These compounds are called isothiocyanates (ITCs), and they are ubiquitous in the plant family Brassicaceae. Precursor compounds called glucosinolates (GSLs) are converted to ITCs via the action of myrosinase enzyme. This thesis presents data relating to numerous a

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Whisman, Curtis D. "Emissivity of rocket plume particulates." Thesis, Monterey, California. Naval Postgraduate School, 1992. http://hdl.handle.net/10945/23876.

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Approved for public release; distribution is unlimited<br>The optical properties of motor aluminum oxide are required inputs to current plume signature prediction codes, such as SIRRM. Accurate predictions are possible only if variations in the particle emissivity due to changes in particle size, contamination, and changing temperature, etc. , are known . This investigation demonstrated a simplified method for determination of the emissivity of rocket motor generated alumina. Plume particulate material was collected on tungsten alloy wire during motor firings. A DC circuit was used

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Kumar, Renjith R. "Singular optimal atmospheric rocket trajectories." Thesis, Virginia Tech, 1986. http://hdl.handle.net/10919/43577.

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<p>Singular subarcs arise in quite a few problems of flight dynamics. The present study is devoted to the specific problem of ascent and acceleration of a vehicle in atmospheric flight in which a variable-thrust arc forms a part of the optimal trajectory. A two-parameter family of singular arcs was generated for time-range-fuel problems of an ascending rocket, using the modelling of Zlatskiy and Kiforenko. The short-term optimality of the singular subarcs has been checked in terms of certain necessary conditions: the classical Clebsch condition, the Kelley condition or the Generalized Legendre

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Fedorchenko, Ilya. "Thermonuclear engines in rocket science." Thesis, National Technical University of Ukraine "Igor Sikorsky Kyiv Polytechnic Institute", 2019. https://er.knutd.edu.ua/handle/123456789/15219.

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The intensive development of rocket science is attracting more and more attention. The creation of thermonuclear engines will take rocket science to a new level and will make longer flights possible. In the future, the use of rockets with thermonuclear engine could even enable an interstellar voyage to the nearest star system, Alpha Centauri. Nowadays scientists are working on creating weaker and correspondingly more compact reactors that can be installed on the rocket board. The main task of the paper is to describe why the use of thermonuclear engines will lead to more efficient space flight

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Vanherweg, Joseph B. R. "HYBRID ROCKET MOTOR SCALING PROCESS." DigitalCommons@CalPoly, 2015. https://digitalcommons.calpoly.edu/theses/1394.

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Hybrid rocket propulsion technology shows promise for the next generation of sounding rockets and small launch vehicles. This paper seeks to provide details on the process of developing hybrid propulsion systems to the academic and amateur rocket communities to assist in future research and development. Scaling hybrid rocket motors for use in sounding rockets has been a challenge due to the inadequacies in traditional boundary layer analysis. Similarity scaling is an amendment to traditional boundary layer analysis which is helpful in removing some of the past scaling challenges. Maintaining g

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Brock, Andrew. "Aerospike Rocket Motor Structural Webbing." DigitalCommons@CalPoly, 2015. https://digitalcommons.calpoly.edu/theses/1355.

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A labscale hybrid rocket motor test stand has been developed for research at Cal Poly. The primary focus of research using this rig has been the development of regenerative cooling techniques using nitrous oxide as coolant and oxidizer, as well as validation of technologies relating to the annular aerospike nozzle. In order to prevent undesirable deflection of the cantilevered spike, a structural stiffening web, referred to as “The Spider,” is proposed. The Spider resembles a three-spoked wheel, with the aerospike held by the inner hub and the chamber walls abutting the outer radius. The Spide

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Wang, Lei. "Investigations into deep cracks in rocket motor propellant models." Thesis, Virginia Tech, 1990. http://hdl.handle.net/10919/42146.

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Star grain configuration design has been widely used in solid rocket applications for several decades. Although a large number of surface cracks are detected in the rocket motor propellants, the mechanism of these cracks is sull not well known due to the complex geometry of the grain. A stress-freezing photoelastic investigation has been performed to study the deep cracks which emanate from the fingertips of the star-shaped cutout cylinders. Using three-dimensional photoelasticity and proper algorithms in fracture mechanics, the stress intensity factors (SIF's) and the stress singularity ord

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Patterson, William Ray. "DEVELOPMENT OF A ROCKET MOTOR TEST SYSTEM AND A STUDY OF HYBRID ROCKET FUEL GRAINS." MSSTATE, 2009. http://sun.library.msstate.edu/ETD-db/theses/available/etd-07062009-120546/.

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A rocket test system was developed and fabricated for the purpose of testing hybrid rocket motors. The test system includes a rocket test stand, load cell, and data acquisition system that is capable of safely and accurately recording thrust data from each burn. This paper documents the test system design and operation. The test system has been used to study the performance results from using multiple types of fuel utilized in hybrid motor systems. The types of hybrid motors used typically have thrust values below 1000 lbf. Along with different fuels, different motor configurations were also u

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Books on the topic "Rocket"

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Ward, Jonathan H. Rocket Ranch. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17789-2.

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Denny, Mark, and Alan McFadzean. Rocket Science. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-28080-2.

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Coulton, Mia. Danny's rocket. MaryRuth Books, 2009.

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Marks, Graham. Renegade rocket. Boxtree, 1993.

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Harris, Colin. The rocket. Oxford University Press, 1985.

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Greene, Melanie. Rocket man. GreeneLeaves, 2014.

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Julian, Baum, ed. Rocket rescue. Dorling Kindersley Book, 2000.

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ill, Ancona George, ed. Richie's rocket. Hampton-Brown Books, 1996.

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Lyon, Tammie, and Lisa Harkrader. Rocket Rivals: Rockets. Boyds Mills & Kane, 2019.

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Rocket Rivals: Rockets. Kane Press, 2019.

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Book chapters on the topic "Rocket"

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Smith, Michael G. "Rocket." In The Spacefaring Earth. Routledge, 2024. http://dx.doi.org/10.4324/9781003494409-4.

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Tewari, Ashish. "Rocket Flight." In Basic Flight Mechanics. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-30022-1_7.

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Walker, John M. "Rocket Immunoelectrophoresis." In Springer Protocols Handbooks. Humana Press, 1996. http://dx.doi.org/10.1007/978-1-60327-259-9_137.

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El-Sayed, Ahmed F. "Rocket Propulsion." In Fundamentals of Aircraft and Rocket Propulsion. Springer London, 2016. http://dx.doi.org/10.1007/978-1-4471-6796-9_11.

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Billingsley, John. "Rocket Science." In Essentials of Dynamics and Vibrations. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-56517-0_13.

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Bahr, Benjamin, Boris Lemmer, and Rina Piccolo. "Rocket Maneuvers." In Quirky Quarks. Springer Berlin Heidelberg, 2016. http://dx.doi.org/10.1007/978-3-662-49509-4_11.

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Walter, Ulrich. "Rocket Fundamentals." In Astronautics. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-74373-8_1.

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Walter, Ulrich. "Rocket Flight." In Astronautics. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-74373-8_2.

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Walter, Ulrich. "Rocket Staging." In Astronautics. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-74373-8_3.

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Sivathanu Pillai, A. "Rocket Principles." In Introduction to Rocket Science and Space Exploration. CRC Press, 2022. http://dx.doi.org/10.1201/9781003323396-4.

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Conference papers on the topic "Rocket"

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Kawasaki, Zen, and Vernon Cooray. "Rocket Triggered Lightning." In 12th International Zurich Symposium and Technical Exhibition on Electromagnetic Compatibility. IEEE, 1997. https://doi.org/10.23919/emc.1997.10784084.

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Solá, A., and P. Solano-López. "Fly a Rocket! Undergraduate rocket science." In 3rd Symposium on Space Educational Activities. University of Leicester, 2020. http://dx.doi.org/10.29311/2020.45.

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BINDER, MICHAEL. "An RL10A-3-3A rocket engine model using the Rocket Engine Transient Simulator (ROCETS) software." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2357.

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de Oliveira Junior, Wilson Luiz, Heloise Assis Fazzolari, Cesar Monzu Freire, and Carlos Alberto de Paiva Carvalho. "6 degrees of freedom simulation of an unguided sounding rocket using Matlab/Simulink." In SAE Brasil 2023 Congress. SAE International, 2024. http://dx.doi.org/10.4271/2023-36-0095.

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<div class="section abstract"><div class="htmlview paragraph">Unguided sounding rockets, also known as sub-orbital rockets, are vehicles that carry scientific experiments and/or sensors to collect data during their trajectory. These rockets lack active control but are capable of traversing the Earth’s atmosphere. It is crucial to thoroughly analyze the flight parameters during the preliminary design phase.</div><div class="htmlview paragraph">The Open Rocket flight simulation software, developed by Sampo Niskanen, is a widely used open-source project. However, it has so

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Tortosa Masbernat, Ernest, Vicente Rubio Juan, Jordi Grau Rifà, et al. "Progress of the development of a two-stage supersonic rocket within a student’s association." In Symposium on Space Educational Activities (SSAE). Universitat Politècnica de Catalunya, 2022. http://dx.doi.org/10.5821/conference-9788419184405.033.

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The Ares mission is part of a student-led project with the aim of developing a two-stage supersonic amateur rocket. This paper discusses the progress since its foundation in 2016 and how it is planned to continue progressing to achieve this objective. Currently, 4 rockets have been built and launched, evolving different aspects of the design and construction process in each one. From the Ares I, a two-stage rocket intended to test the electronics and the structure, the mission has evolved into designing the Phobos, a rocket whose aim is to compete in European Rocketry Challenges for universiti

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KNIFFEN, R., BEVIN MCKINNEY, and PAUL ESTEY. "Hybrid rocket development at the American Rocket Company." In 26th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2762.

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Balepin, Vladimir V., Makoto Yoshida, and Kenjiro Kamijo. "Rocket Based Combined Cycles for Single Stage Rocket." In Aerospace Atlantic Conference & Exposition. SAE International, 1994. http://dx.doi.org/10.4271/941166.

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Naumann, Karl W., Matthias Berndl, Ludwig Eineder, et al. "A First Stage Solid Propellant Rocket Motor for Sounding Rockets." In AIAA Propulsion and Energy 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-3692.

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Casalino, Lorenzo, and Dario Pastrone. "A Parametric Analysis of Hybrid Rocket Motors for Sounding Rockets." In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-4544.

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Guo, Zhenrui. "A Simulation Program that Controls Rockets Using AI Trained with Machine Learning." In 12th International Conference on Digital Image Processing and Vision. Academy & Industry Research Collaboration, 2023. http://dx.doi.org/10.5121/csit.2023.131319.

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Launching rockets is a costly and complex task that is prone to a high rate of failure. To help address these challenges, the need for simulations to help emulate reality when developing rockets is crucial to making sure the cost overhead stays as low as possible. Our rocket AI seeks to tackle this challenge through the use of machine learning and a series of emulated phases to demonstrate an AI’s ability to properly operate a rocket. The primary challenge throughout the development of the rocket’s AI is the need to introduce and train for unexpected situations, which is done by training for a

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Reports on the topic "Rocket"

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Leathe, Nicholas. NASA Sounding Rocket Payload. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1416483.

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Keaton, P. W. Low-thrust rocket trajectories. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5985829.

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Keaton, P. W. Low-thrust rocket trajectories. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/6237070.

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Sanders, III, Sells George A., and Ray. Mini-Rocket User Guide. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada471792.

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Sanders, III, Sells George A., and Ray. Mini-Rocket User Guide. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada472173.

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Resendiz Lira, Pedro, and Gian Delzanno. Rocket 3D CPIC Simulations. Office of Scientific and Technical Information (OSTI), 2025. https://doi.org/10.2172/2568632.

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ARMY MATERIEL COMMAND ALEXANDRIA VA. Logistics Complete Round Charts: Grenades, Mines, Pyrotechnics, Rockets, Rocket Motors, Demolition Material. Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada213109.

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Heimer, Brandon Walter, Jason Christian Reinhardt, and Lynne Schleiffarth Burks. The Rocket Test Case Study. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1425724.

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Lawrence, Timothy J. Nuclear Thermal Rocket Propulsion Systems. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada430931.

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Evans, Amanda Christine. From Biowaste to Rocket Fuel. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1532692.

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