Relevant bibliographies by topics / Rocketry in art

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Rocketry in art'

Author: Grafiati
Published: 4 June 2021
Last updated: 28 July 2025

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Journal articles on the topic "Rocketry in art"

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Wlodkowski, Paul. "Engineering of the Highest Caliber: Kazimierz Siemienowicz and the Culmination of the Military Revolution." Studia Historiae Scientiarum 21 (August 26, 2022): 25–58. https://doi.org/10.4467/2543702XSHS.22.002.15968.

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The interregnum between the death of Galileo and the publication of Newton’s Principia produced great advances in military science and technology. Particularly noteworthy are Kazimierz Siemienowicz’s contributions to artillery and to the field of rocketry. The dominating nature of these weapon systems remain as relevant today as it did in 1650 with the publication of his opus, The Great Art of Artillery. Rocket technology defines power relations, whether fired indiscriminately across a national border or positioned menacingly in a silo as an intercontinental ballistic missile. Siem
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Dong, Xiaobo, Xiaoqing Wang, Yongde Liu, and Xiaorong Wang. "Development and preliminary testing of a temporally controllable weather modification rocket with spatial seeding capacity." Atmospheric Measurement Techniques 17, no. 18 (2024): 5551–59. http://dx.doi.org/10.5194/amt-17-5551-2024.

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Abstract. Current weather modification rockets with a single operation mode, limited operating height, and fixed and uncontrollable operating time cannot achieve seeding in different layers, stages, and quantities for different cloud systems. Therefore, a temporally controllable weather modification rocket with spatial seeding capability is developed in this study. This new rocket features an electronic fuse-controlled intelligent ignition system, with eight channels of ignition tube outputs. Additionally, carrier wave communication technology is incorporated to set the seeding time for eight
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Shubov, Mikhail. "Electric Rocket Launcher Aircraft—Drone-Launched Short Range Rocket System." Aerospace 10, no. 6 (2023): 514. http://dx.doi.org/10.3390/aerospace10060514.

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This paper is concerned with the idea of a significant improvement of state-of-the-art short-range rockets by means of using rocket artillery systems. Such a system consists of a rocket launcher aircraft (RLA) and a drone-launched short range rocket (DLSRR). An RLA is a reusable first stage of a military rocket. A DLSRR is the expendable second stage, which flies to the target. RLA-DLSRR systems have not yet been built, but they have been described in previous works by the author. State-of-the-art rocket systems are completely expendable and, hence, extremely expensive. No rocket artillery sys
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Mathews, Logan T., Hunter J. Pratt, Mark C. Anderson, and Kent L. Gee. "Directivity and sound power of rockets: A comparative analysis of source characteristics and their implementation into a predictive model." Journal of the Acoustical Society of America 154, no. 4_supplement (2023): A347. http://dx.doi.org/10.1121/10.0023752.

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Fundamental jet and rocket noise modeling includes quantifying the acoustic power and directivity characteristics of the source. While many attempts have been made to define a model for the sound power and directivity of jets and rockets, many of these models have been based on flawed measurements or methodologies. This paper presents the directivity and sound power characteristics as obtained from launched rockets. The results are compared with those in the literature. The directivity and sound power properties are used in a standard source model for rocket noise, and the resulting prediction
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Khorolskyi, M. S., and S. O. Bigun. "Performance of interface hoses for thermal conditioning system of "Cyclon-4" space rocket in extreme conditions." Kosmìčna nauka ì tehnologìâ 27, no. 4 (2021): 11–20. http://dx.doi.org/10.15407/knit2021.04.011.

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This article contains the analysis of the performance of interface hoses for the thermal conditioning system of a Cyclone-4 space rocket in extreme operating conditions. thermal conditioning system interfaces with rubber hoses must ensure a tightness of a hose at a rocket’s inlet with easy detachment, involving little to no force impact on the rocket during its start on its one end, and rigid connection with a pipeline of the thermal conditioning system ground part, ensuring the hose tightness and retaining after the launch of a rocket on its other end, under any abnormal operating conditions.
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Milne, Benjamin, Sean Samson, Robert Carrese, Alessandro Gardi, and Roberto Sabatini. "High-Fidelity Dynamics Modelling for the Design of a High-Altitude Supersonic Sounding Rocket." Designs 7, no. 1 (2023): 32. http://dx.doi.org/10.3390/designs7010032.

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The accurate modelling and simulation of vehicle dynamics is a fundamental prerequisite for the design and experimental flight testing of aerospace vehicles. In the case of high-altitude supersonic sounding rockets, it is critically important to produce realistic trajectory predictions in a representative range of operational and environmental conditions as well as to produce reliable probability distributions of terminal locations. This article proposes a methodology to develop high-fidelity flight dynamics models that accurately capture aeroelastic, turbulence, atmospheric and other effects
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Pilger, Christoph, Patrick Hupe, and Peter Gaebler. "Worldwide detection of rocket launches for space missions using International Monitoring System infrasound arrays." Journal of the Acoustical Society of America 154, no. 4_supplement (2023): A347. http://dx.doi.org/10.1121/10.0023754.

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The signals of rocket launches can be detected at infrasound arrays in thousands of kilometers distance. We use microbarometer arrays, which are part of the International Monitoring System (IMS) for the Comprehensive Nuclear-Test-Ban Treaty (CTBT), to identify and characterize rocket launches all over the world. We studied more than 1000 launch events for space missions and their infrasonic signatures. Even small-lift launch vehicles such as Electron rockets starting from New Zealand with payloads of only a few hundreds of kilograms, e.g., for small satellites, can regularly be detected by one
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Ioannis, Michaloudis, and Matthew van Roden. "Spirited Skies project: Silica Aerogel in Art and Design Applications." MRS Advances 2, no. 57 (2017): 3491–97. http://dx.doi.org/10.1557/adv.2017.349.

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ABSTRACTThis comparative study on two interdisciplinary artistic practices aims to improve public perception of scientific research and to facilitate informed decision making regarding climate change and how it affects everyday life. It also hopes to break down (or bridge?) the isolated silos of Art and Science, by emphasizing the role of imagination as a tool of creation and innovation in the new economies of the 21st century. Notwithstanding the ephemeral appearance of the super-light nanomaterial silica aerogel used by Ioannis Michaloudis (Michalous) in his sculptures, the longevity of some
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Rasband, Reese, and Alan T. Wall. "A look into far-field rocket noise modeling: Approaches and potential sources of error." Journal of the Acoustical Society of America 154, no. 4_supplement (2023): A346. http://dx.doi.org/10.1121/10.0023751.

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In recent years, rocket launches have elevated from novelty to being seen as means of transportation, exploration, and delivery. Defense, commercial, and public sectors are looking to increase their cadence in missions and ability to perform them. Like airports before them, spaceports are being developed and regulated. Much research has been done in rockets as a noise source, and how they may affect communities, structures, and wildlife. The most common approach for modeling the far-field rocket noise relies heavily on NASA SP-8072 and work done by Dr. Sally McInerny, a NASA researcher. The ap
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Gee, Kent L., Logan T. Mathews, Bradley McLaughlin, Mark C. Anderson, Daniel Edgington-Mitchell, and Grant W. Hart. "Rocket noise: What does it mean for Australian spaceports?" Journal of the Acoustical Society of America 154, no. 4_supplement (2023): A346. http://dx.doi.org/10.1121/10.0023749.

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As the global space industry expands, rockets are being launched from an increasing number of spaceports, including in Australia. As launch cadence increases to meet demand for space access and as vehicle optimization for weight and cost reduction becomes more pressing, noise has the potential to create harmful impacts—from vehicle vibroacoustic loading to expanded environmental footprint. Using data from recently measured launches, this presentation reviews rocket noise generation and propagation fundamentals and discusses some of these impacts. As small- and medium-payload orbital rocket lau
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Dissertations / Theses on the topic "Rocketry in art"

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Remes, Eriksson Åsa. "Framtagandet av gestaltningsskiss i sjukhusmiljö med sten och stenpartiväxter som utgångsmaterial." Thesis, Högskolan i Gävle, Avdelningen för elektronik, matematik och naturvetenskap, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:hig:diva-18644.

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Enligt forskning har riktig natur och bilder av natur en avstressande effekt på människor i sjukhusmiljö. Stenpartier byggs ofta för att simulera naturliga förhållanden och kan upplevas som en tredimensionell landskapsmålning som förändras med årstidens växlingar. Syftet med denna studie är att komma fram till en gestaltningsskiss med hjälp av sten och stenpartiväxter. Gestaltningen tänkta plats är utanför Gävle sjukhus. Fokus har lagts på stenpartiets uppbyggnad, växternas krav och anpassningen till sjukhusmiljön. För att ta reda på ett stenpartis uppbyggnad och stenpartiväxters krav på växtm
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Castro, Gonzalo. "We are sudamerican rockers, acordes de una época." Tesis, Universidad de Chile, 2008. http://repositorio.uchile.cl/handle/2250/170527.

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Memoria para optar al título de Periodista<br>Ser músico, en general, nunca ha sido una tarea simple en Chile, pero ser de rock y en una década de agitación política era casi una locura. Todas las bandas que forman parte de la presente investigación responden en esencia a la gesta heroica de crear música en condiciones sociales complicadas que jugaban en contra y en un periodo donde además el profesionalismo debió partir de cero. “We are Sudamerican Rockers” desea exponer la historiografía musical de una época compleja. Pero antes de comenzar es necesario aclarar que siempre que se habla d
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Judson, Michael I. Jr. "Direct Electrical Arc Ignition of Hybrid Rocket Motors." DigitalCommons@USU, 2015. https://digitalcommons.usu.edu/etd/4149.

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Hybrid rockets motors provide distinct safety advantages when compared to traditional liquid or solid propellant systems, due to the inherent stability and relative inertness of the propellants prior to established combustion. As a result of this inherent propellant stability, hybrid motors have historically proven dicult to ignite. State of the art hybrid igniter designs continue to require solid or liquid reactants distinct from the main propellants. These ignition methods however, reintroduce to the hybrid propulsion system the safety and complexity disadvantages associated with traditional
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Krolak, Matthew Joseph. "Optimization of a magnetoplasmadynamic arc thruster." Link to electronic thesis, 2007. http://www.wpi.edu/Pubs/ETD/Available/etd-042607-155701/.

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Bennett, Steven Russell. "Control and Stability of Upper Stage Launch Vehicle With Hybrid Arc-Ignition Attitude Control System." DigitalCommons@USU, 2019. https://digitalcommons.usu.edu/etd/7518.

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The Utah State University Propulsion Research Laboratory (USUPRL) has recently made significant developments in the area of hybrid rocket systems. This type of propulsion system incorporates a solid fuel and a gas or liquid oxidizer. Hybrid rocket systems are known for their inherent safety, reliability, and restart capability. Over the last several years, the USUPRL has successfully built and tested a hybrid rocket system comprising acrylonitrile butadiene styrene (ABS) plastic and gaseous oxygen (GOX). The system was demonstrated to be fully functional during ground, vacuum, and sub-orbital
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Hetreed, Christopher F. "Internal flow investigation of an aft finocyl grain configuration in a solid rocket motor." Thesis, Virginia Tech, 1989. http://hdl.handle.net/10919/46038.

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<p>Cold-flow tests were conducted in mediums of air and water to investigate the internal flow field about the nozzle region of a proposed solid rocket motor (SRM) configuration that would potentially replace the current external boosters on NASA's Space Shuttle. One-eighth-scale clear acrylic models of the proposed submerged aft-dome and aft finned grain elements were constructed to simulate the aft segment of the SRM at ignition and 35 seconds into the firing sequence. Pressure, velocity, and turbulence profiles were obtained during cold air testing, while air bubbles and dye were used f
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Graur, Mina. "An Anarchist "Rabbi" : the life and teachings of Rudolf Rocker /." New York : Jerusalem : St. Martin's press ; Magnes press, 1997. http://catalogue.bnf.fr/ark:/12148/cb39259083p.

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Anderson, Leslie J. "Ponies and Rocketships: Poems For America, A Collection of Selected Poems." Ohio University / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1307492733.

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Godwin, Matthew. "The Skylark rocket : British space science and the European space research organisation, 1957-1972 /." Paris : Beauchesne, 2007. http://catalogue.bnf.fr/ark:/12148/cb411905977.

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Weyer, Robert Bernhard. "Investigation of the functioning of a liquefied-gas micro-satellite propulsion system." Thesis, Stellenbosch : Stellenbosch University, 2003. http://hdl.handle.net/10019.1/49765.

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Thesis (MScEng)--University of Stellenbosch, 2003.<br>ENGLISH ABSTRACT: The focus of this thesis is on the investigation of the functioning of a liquefied-gas thruster. Such a thruster could be used to provide secondary propulsion to a microsatellite in orbit. A general overview of the need for thrusters in micro-satellites is put forward in the introduction. Motivation for deciding to investigate a liquefied-gas system is presented. Recent developments in the field of micro-satellites are discussed as well as their relevance to the project undertaken. Fundamental background theory rel
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Books on the topic "Rocketry in art"

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Chun, Clayton K. S. Thunder over the horizon: From V-2 rockets to ballistic missiles. Praeger Security International, 2006.

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Bergin, Mark. You Can Draw Rockets. Gareth Stevens Publishing, 2012.

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A, Mantenieks Maris, and United States. National Aeronautics and Space Administration., eds. Performance and lifetime assessment of MPD arc thruster technology. National Aeronautics and Space Administration, 1988.

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J, Sovie Amy, Haag Thomas W, and United States. National Aeronautics and Space Administration., eds. Arcjet nozzle design impacts. National Aeronautics and Space Administration, 1989.

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Foundation, FLAG Art, ed. Wall rockets. Flag Art Foundation, 2008.

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A, Wasel Robert, and United States. National Aeronautics and Space Administration., eds. The NASA electric propulsion program. National Aeronautics and Space Administration, 1987.

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Center for Book Arts (New York, N.Y.), ed. Peace, love and rockets. Center for Book Arts, 2012.

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Center, Rockefeller, Gagosian Gallery, Public Art Fund (New York, N.Y.), and Tishman Speyer, eds. Jeff Koons: Split-rocker. Gagosian Gallery, 2014.

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David, Miller. Soviet rocket forces. Rourke Publications, 1988.

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Hills, Tad. Rocket veut lire. Éditions Scholastic, 2011.

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Book chapters on the topic "Rocketry in art"

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Mickelwait, A. B. "Rocketry." In Contemporary Geodesy: Proceedings of a Conference Held at the Harvard College Observatory-Smithsonian Astrophysical Observatory, Cambridge, Massachusetts, December 1-2, 1958. American Geophysical Union, 2013. http://dx.doi.org/10.1029/gm004p0053.

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Spadoni, Aldo. "Hardware Art: Space Art Meets Rocket Science." In The Beauty of Space Art. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-49359-2_10.

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Sagliano, Marco, David Seelbinder, and Stephan Theil. "Autonomous Descent Guidance via Sequential Pseudospectral Convex Programming." In Autonomous Trajectory Planning and Guidance Control for Launch Vehicles. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-0613-0_5.

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AbstractThis chapter expands our development of an autonomous descent guidance algorithm which is able to deal with both the aerodynamic descent and the powered landing phases of a reusable rocket. The method uses sequential convex optimization applied to a Cartesian representation of the equations of motion, and the transcription is based on the use of hp pseudospectral methods. The major contributions of the formulation are a more systematic exploitation and separation of convex and non-convex contributions to minimize the computation of the latter, the inclusion of highly nonlinear terms re
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Raley, Rita, and Russell Samolsky. "Rocket Theory." In Left Theory and the Alt-Right. Routledge, 2023. http://dx.doi.org/10.4324/b23360-8.

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Dron’, Mykola, Andrii Dreus, Ludmila Dubovik, and Olena Kositsyna. "Thermodynamic assessment of the possibility of using polymeric materials in promising launch vehicles." In INNOVATIVE MATERIALS AND TECHNOLOGIES IN FUNCTIONAL ENGINEERING SYSTEMS. TECHNOLOGY CENTER PC, 2023. https://doi.org/10.15587/978-617-7319-96-1.ch4.

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One of the ways to reduce the cost of space launches for the operational launch of constellations of satellites into the Earth's orbit is the creation of targeted launch vehicles based on light and ultralight class rockets. The solution to this problem lies, among other things, in the area of development and application of new structural materials. The presented work considers the possibility of using polymers on the one hand as a structural material for creating the hulls of launch vehicles, and on the other hand as solid fuel for rocket engines. Research is related to the development of a ne
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Ma, Qingtian, Cungui Yu, Guanglei Li, Cheng Zhou, Shuang Liu, and Junyi Ma. "Simulation Study on Driving Dynamic Characteristics of a Light Rocket Launcher." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-1876-4_26.

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AbstractTaking a light rocket launcher as the research object, based on random road excitation and applying the theory of multi-rigid-body system dynamics, the multi-body dynamics model of a light rocket launcher is established, and its driving dynamic characteristics are studied. Considering the load-bearing characteristics of leaf spring and the use of tires, the driving dynamics simulation of light rocket launcher on C-class virtual road is carried out. Considering the vibration impact of the road surface on the rocket launcher, the vibration characteristic results of the rocket launcher ar
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Bryant, D. A. "Rocket Studies of Particle Structure Associated with Auroral Arcs." In Physics of Auroral Arc Formation. American Geophysical Union, 2013. http://dx.doi.org/10.1029/gm025p0103.

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Fiedler, Torben, Joachim Rösler, Martin Bäker, et al. "Mechanical Integrity of Thermal Barrier Coatings: Coating Development and Micromechanics." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_19.

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Abstract To protect the copper liners of liquid-fuel rocket combustion chambers, a thermal barrier coating can be applied. Previously, a new metallic coating system was developed, consisting of a NiCuCrAl bond-coat and a Rene 80 top-coat, applied with high velocity oxyfuel spray (HVOF). The coatings are tested in laser cycling experiments to develop a detailed failure model, and critical loads for coating failure were defined. In this work, a coating system is designed for a generic engine to demonstrate the benefits of TBCs in rocket engines, and the mechanical loads and possible coating fail
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Campos, L. M. B. C., and P. J. S. Gil. "On the Trajectory of Rockets in the Atmosphere." In Progress in Industrial Mathematics at ECMI 2008. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-12110-4_119.

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Wyckoff, P. H. "The Rocket as a Research Vehicle." In Geophysics and the IGY: Proceedings of the Symposium at the Opening of the International Geophysical Year. American Geophysical Union, 2013. http://dx.doi.org/10.1029/gm002p0102.

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Conference papers on the topic "Rocketry in art"

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Gomez Monroy, Luis Fernando, and Antonio De Jesús Flores Moreno. "Establishing a Foundation for Rocketry Advancement in Mexico: Development of a Hybrid Rocket Engine." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0183.

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Bogale, Zelalem, and Eden Habteslasie. "Development and Testing of an Electrically-Driven Centrifugal Pressurization System for Hybrid Rockets in Rocket Propulsion." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0115.

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Weekes, Madison, Zoran Vulovic, and Ethan Athos. "Adaptive Optimal Control System Design for Amateur Rocketry." In 52nd IAF Student Conference, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078379-0009.

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Pérez Reyes, Diego, Isaac Alejandro Pimentel Morales, and Nuria Hernández Alás. "Advancing Experimental Rocketry: FDM-Enabled Ceramic Nozzles for Low-Budget Experimental Propellants." In IAF Materials and Structures Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078369-0153.

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Gomez Monroy, Luis Fernando, Luis Angel Garcia Sanchez, and Alberto Garcia Sanchez. "En El Tule Aeroespacial: Fostering STEAM Education Through Sustainable Experimental Rocketry Outreach." In IAF Space Education and Outreach Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078378-0134.

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Cocirla, Gianluca, Marco Grossi, Daniele Bianchi, et al. "Three Dimensional and Multiphase Simulations of Aft-Finocyl Solid Rocket Motors." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0194.

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Vázquez, Angel, Moises Tolentino Angeles, Julio Morales, Alejandro Jiménez Gómez, and Joshua Anastacio. ""Chaac": Harnessing Machine Learning for Intelligent Combustion Control and Sustainable Propellants in Liquid Propellant Rocketry." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0213.

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Yamashiro, Ryoma, Takao Munenaga, Yoshio Nunome, et al. "Subsystem and System Test Results of the 4-Ton Class Rocket Engine for Rocket Startups." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0012.

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Fernandez-Tous, Marcos, Michael Dodge, and Preeti Nair. "Nuclear Powered Rockets: Legal Issues and Perspectives." In IISL Colloquium on the Law of Outer Space, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078384-0040.

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Morales Benítez, Claudio Antonio, Elias Basaldua, Ángel Perez, et al. "Improving Rocket Nozzle Efficiency with Rough Surfaces." In IAF Space Propulsion Symposium, Held at the 75th International Astronautical Congress (IAC 2024). International Astronautical Federation (IAF), 2024. https://doi.org/10.52202/078371-0105.

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Reports on the topic "Rocketry in art"

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Berlinger, C. H. REVIEW OF EMERGENCY DIESEL GENERATOR ROCKER ARM CAPSCREWS. Office of Scientific and Technical Information (OSTI), 1985. http://dx.doi.org/10.2172/1086285.

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Garner, Trevor W. ARL Support of NRL Rocket Experiments to Investigate Ionospheric Phenomena. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada529149.

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BALYSH, A. N., and O. B. CHIRICOVA. SOME ASPECTS OF THE DEVELOPMENT OF ROCKET WEAPONS IN THE USSR IN THE 20-40S OF THE XX CENTURY. Science and Innovation Center Publishing House, 2022. http://dx.doi.org/10.12731/2077-1770-2021-14-1-2-91-102.

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The aim of the article. Establishment and development of the USSR rocket weapons for the period of the New Economic Policy and industrialization is one of the most interesting and poorly researched problem of the USSR military industry. The USSR first researches in the field of rocket weapons and ammunition creation, their features and results are poorly investigated by national historical science and just they are observed in the paper. Methodology. General principles of historism and objectivity are the theoretical-methodological base of this work. Author also use special historical methods:
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ADAS, RSK. Nitrate Surveillance Monitoring Program (Annual Report May 2021 - March 2022). Food Standards Agency, 2022. http://dx.doi.org/10.46756/sci.fsa.uau489.

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Every Member State is required to monitor and report levels of nitrate in specified foodstuffs as part of the European Commission regulation and the UK also requires this information as part of the collection of data to support the review of retained EU law in the UK and inform the setting of policy around maximum nitrate levels. The requirement to carry out monitoring for nitrate in lettuce, spinach and rocket is being met by the UK Nitrate Surveillance Programme. Results are presented for the period between 1st April 2021 and 31st March 2022. A total of 202 samples were collected within the
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Shkurupiy, Valeria, and Nikita Budnyi. A priori estimation of instrumental error of energy characteristics of an electric rocket engine. Baltic State Technical University “VOENMEH” named after D.F.Ustinov, 2023. http://dx.doi.org/10.12731/edn:dkwobv.

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In this work, the power of the calculated electric rocket engine (ERE) requires thrust, specific impulse, and efficiency. ERE thrust measurement is interesting enough to achieve smallness of rapid growth. Specific impulse and efficiency are measured using laboratory methods. For this reason, one should naturally approach the choice of design parameters and the composition of the measuring system. One of the synthesis products can be the minimization of measurement errors. The paper approaches an approach to a priori instrumental estimation of the error determination, which may be useful in the
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Willson. L51709 Development-Test Electronic Gas Admission for Large Bore Engines. Pipeline Research Council International, Inc. (PRCI), 1994. http://dx.doi.org/10.55274/r0010114.

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The pipeline industry uses over 8,000 large bore engines in gas transmission/compression service". These engines are typically gas fueled and spark ignited. Some early versions of the engines are piston scavenged, but most are turbocharged. Some models, especially those equipped for lean burn operation, utilize pre-combustion chambers for enhanced ignition. Typically, the gaseous fuel is admitted directly into the top of the engine combustion chamber by a cam-operated, mechanical gas admission valve (MGAV). The MGAV is operated by an engine driven cam, cam follower, push rod, and rocker assemb
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Barker, Amanda, Jay Clausen, Thomas Douglas, Anthony Bednar, Christopher Griggs, and William Martin. Environmental impact of metals resulting from military training activities : a review. Engineer Research and Development Center (U.S.), 2022. http://dx.doi.org/10.21079/11681/43348.

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The deposition of metals into the environment as a result of military training activities remains a longterm concern for Defense organizations across the globe. Of particular concern for deposition and potential mobilization are antimony (Sb), arsenic (As), copper (Cu), lead (Pb), and tungsten (W), which are the focus of this review article. The fate, transport, and mobilization of these metals are complicated and depend on a variety of environmental factors that are often convoluted, heterogeneous, and site dependent. While there have been many studies investigating contaminant mobilization o
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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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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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METHOD OF IMPERFECTION RANDOM FIELD CONSTRUCTION FOR WELDED CYLINDRICAL SHELL BASED ON SMALL SAMPLE. The Hong Kong Institute of Steel Construction, 2025. https://doi.org/10.18057/ijasc.2025.21.1.6.

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The initial geometrical imperfections of thin-walled cylindrical shell structures are important factors that cause the actual bearing capacity of such products to deviate from the theoretical value. In recent years, with the development of digital image measurement technology, it is possible to obtain geometric imperfections(GIs) through the measurement of the real geometric shape of the product, and it is possible to accurately predict the structural load-bearing capacity by considering the imperfections. On this basis, the initial GIs random field can then be considered to carry out thin-wal
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