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1

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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7

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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8

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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9

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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10

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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11

Zhou WuZhong and Chen Xiaoyan. "A SURVEY OF ROCKERY ART HISTORY IN TRADITIONAL CHINESE GARDENS." Acta Horticulturae, no. 881 (November 2010): 287–94. http://dx.doi.org/10.17660/actahortic.2010.881.38.

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12

Pylypenko, O. V., O. D. Nikolayev, N. V. Khoriak, I. D. Bashliy, and S. I. Dolgopolov. "Dynamic processes in solid rocket motors and their interaction with rocket structure vibrations: the state of the art and current problems." Technical mechanics 2023, no. 1 (2023): 3–13. http://dx.doi.org/10.15407/itm2023.01.003.

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The most critical operating conditions of solid rocket motors (SRMs) are often due to the development of dynamic processes characterized by excess values of operating parameters. Pressure surges and a sharp increase in the combustion product temperature may impair the strength of the combustion chamber structure, cause its failure, and lead to critical conditions of the motor operation, up to extinguishing the propellant combustion in the motor. It is shown that both in steady and in unsteady operating conditions of an SRM, dynamic processes in its combustion chamber feature a complex interrel
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13

Rao, B. N., D. Jeyakumar, K. K. Biswas, S. Swaminathan, and E. Janardhana. "Rigid body separation dynamics for space launch vehicles." Aeronautical Journal 110, no. 1107 (2006): 289–302. http://dx.doi.org/10.1017/s0001924000013166.

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Abstract This paper presents a systematic formulation for the simulation of rigid body dynamics, including the short period dynamics, inherent to stage separation and jettisoning parts of a satellite launcher. This also gives a review of various types of separations involved in a launch vehicle. The problem is sufficiently large and complex; the methodology involves iterations at successively lower levels of abstraction. The best choice to tackle such problems is to use state-of-the-art programming technique known as object oriented programming. The necessary classes have been identified to re
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14

Hart, Grant W., Kent L. Gee, and Mylan R. Cook. "Updated frequency-dependent directivity indices for large solid rocket motors." Journal of the Acoustical Society of America 153, no. 3_supplement (2023): A41. http://dx.doi.org/10.1121/10.0018084.

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For many years, empirical models for rocket noise radiation relied on the directivity indices published in NASA SP-8072 (K. Eldred, 1971). Because these indices had known issues, NASA led a campaign to update the indices using a Space Shuttle reusable solid rocket motor (RSRM). The RSRM measurements, involving a polar arc at a radius of about 80 nozzle exit diameters, resulted in updated directivity indices (Haynes and Kenny, AIAA 2009–3160). However, because the arc origin was placed at the nozzle exit plane, James et al. [Proc. Mtgs. Acoust., 18, 040008 (2012)] corrected the low-frequency in
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15

Sukmana, Septian Enggar, and Ely Nur Rahayu. "Agen Otonom Untuk Ketepatan Penembakan Pada Game Roket Berbasis Ant Colony Optimization." Applied Technology and Computing Science Journal 3, no. 1 (2020): 58–63. http://dx.doi.org/10.33086/atcsj.v3i1.1587.

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ACO berbasis klasifikasi diterapkan pada game Rocket Tank untuk membantu karakter rocket dalam menembak target (tower) secara tepat. Pada paper ini, roket berfungsi sebagai sarang semut dan tower sebagai sumber makanan. Agen semut dijalankan secara acak dan berjalan menemukan sumber makanan. Sumber makanan yang ditemukan didefinsikan sebagai target yang harus ditembak, dasar dari penentuan sumber makanan adalah jumlah bobot feromon yang terkumpul tanpa nilai jarak. Implementasi yang dilakukan pada paper ini adalah membandingkan penerapan ACO berbasis klasifikasi (melibatkan bobot feromon pada
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16

Li, Wen, Wei Duan, and Qu Shi. "Song Dynasty Garden Art and its Inspiration on the Modern Urban Landscape." Applied Mechanics and Materials 744-746 (March 2015): 2206–11. http://dx.doi.org/10.4028/www.scientific.net/amm.744-746.2206.

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Chinese garden art originates from Shang and Zhou Dynasties,drives to maturity in Song Dynasty nurtured by the renovation and development of Wei, Jin, Sui, Tang, Northern and Southern Dynasties. Affected by the situation of valuing literary talent above martial arts, Song Dynasty garden art made a great progress in the aspect of thinking, architecture, plants, rockery and layout of waters, the interests and artistic of paintings and poems became the most notable characteristic of gardens built in Song dynasty. Its space principle and aesthetics taste are totally different from the western gard
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17

Vaulin, S. D., and K. I. Khazhiakhmetov. "The State-of-the-Art and Prospects of Aerospike Engines." Proceedings of Higher Educational Institutions. Маchine Building, no. 10 (739) (October 2021): 74–83. http://dx.doi.org/10.18698/0536-1044-2021-10-74-83.

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Currently, there is a worldwide trend of growing interest in projects aimed at reducing the cost of spacecraft launches. The search for solutions to this topical issue reveals new requirements for the rocket engines. However, existing rocket engines are incapable of fully meeting modern requirements. Consideration of new technical solutions indicates the prospects of using aerospike engines, which have the property of self-regulation and can operate with optimal flow expansion throughout the entire operation. This property allows this type of engine to be used as a propulsion system for single
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18

McDermott, Ryan M., Jitendra S. Tate, and Joseph H. Koo. "Exploration of a new affordable thermal protection system utilizing 2.5D silica/polysiloxane composite." Journal of Composite Materials 56, no. 5 (2021): 685–98. http://dx.doi.org/10.1177/00219983211038622.

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Ablative materials are used as thermal protection systems (TPS) for reentry vehicles and solid rocket motor (SRM) nozzle applications. Phenolic and cyanate ester are the state-of-the-art (SOTA) resin systems used in many of the ablative composites today, including MX-2600 (silica/phenolic) from Cytec Solvay Group. While these ablatives have worked well, more demanding requirements drive the need for affordable lightweight advanced composites capable of handling high heat fluxes with minimal mass loss. These advanced ablative composites result in lighter reentry heat shields and solid rocket mo
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19

Zuo, Tianhao. "Designs, Simulations, and Products for Rocket Engines." Highlights in Science, Engineering and Technology 48 (May 16, 2023): 186–91. http://dx.doi.org/10.54097/hset.v48i.8330.

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As a matter of fact, rocket engine technology has developed rapidly in the last 100 years, which plays a crucial role for stellar travelling and detection for astrophysics usages. To be specific, different models, designs and simulation computer software had been developed in order to investigate and explore the dynamic process of the engines as well as evaluate the effectiveness and ability of the rocket engines. With this in mind, this paper gives a basic description of the designs, simulations, and products for rocket engines. In detail, this study will include description of four basic des
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20

Kimer, Nina, Christian Mortensen, and Lise Hobolth. "Editorial: non‐selective beta blockers—in and out of circulation." Alimentary Pharmacology & Therapeutics 53, no. 5 (2021): 632–33. http://dx.doi.org/10.1111/apt.16199.

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DeWinter, Jennifer, Ken S. McAllister, and Judd Ethan Ruggill. "Evoking the Inexpressible: The Fine Art and Business of Games." Eludamos: Journal for Computer Game Culture 4, no. 1 (2010): 109–15. http://dx.doi.org/10.7557/23.6119.

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This interview is excerpted from a series we conducted in early 2010 with Brian J. Moriarty, Professor of Practice at Worcester Polytechnic Institute (WPI). Moriarty has been developing games for the better part of 30 years, and has worked for Analog, Infocom, LucasArts, Rocket Science, Mpath, Hearme, Skotos Tech, and ImaginEngine. He has produced a host of critically and commercially acclaimed titles, including Wishbringer, Trinity, Beyond Zork, and Loom, which earned MacWorld's Adventure Game of the Year in 1990.
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22

Hedenborg White, Manon. "Magic in Art, Poetry, and Biography." Religion and the Arts 28, no. 1-2 (2024): 133–69. http://dx.doi.org/10.1163/15685292-02801005.

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Abstract The article analyzes four works of poetry and illustration produced by the artist, poet, and occultist Marjorie Cameron (1922–1995) in the 1950s and 1960s. Widow of rocket scientist and occultist John “Jack” Whiteside Parsons (1914–1952), an early follower of Aleister Crowley’s (1875–1947) religion Thelema, Cameron was also a friend and collaborator of Beat artist Wallace Berman (1926–1976) and avant-garde filmmaker Kenneth Anger (1927–2023). In the 1950s and 1960s, Cameron delved deeply into Crowley’s magical writings alongside those of comparative mythologist Joseph Campbell (1904–1
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Sasso, Roula, and Don Rockey. "Editorial: non‐selective beta blockers—in and out of circulation. Authors' reply." Alimentary Pharmacology & Therapeutics 53, no. 5 (2021): 634–35. http://dx.doi.org/10.1111/apt.16242.

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Machovec, Martin. "Czech Underground Musicians in Search of Art Innovation." East Central Europe 38, no. 2-3 (2011): 221–37. http://dx.doi.org/10.1163/174552411x600103.

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AbstractThe Czech underground culture of the 1970s and 1980s has so far been widely acknowledged for its contribution to the development of the human rights movement in the country, especially as a predecessor and fellow-traveller of Charta 77. So have been some of the underground rock musicians (The Plastic People of the Universe) and some of the poets and writers (e.g. Egon Bondy, I. M. Jirous, Pavel Zajíček, Jáchym Topol). However, as a result of vivid cooperation within the underground “ghetto” between poets, writers, philosophers, musicians and representatives of fine arts, the undergroun
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Schwoch, James. "Satellites, rocketry, security and space policy: a comparative history?" Historical Journal of Film, Radio and Television 18, no. 2 (1998): 295–99. http://dx.doi.org/10.1080/01439689800260191.

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Kovalenko, N. E., and A. A. Vnukov. "Application of electric thrusters in a spacecraft propulsion system." Spacecrafts & Technologies 6, no. 2 (2022): 83–89. http://dx.doi.org/10.26732/j.st.2022.2.02.

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The place of electric rocket thrusters in a spacecraft propulsion system is pointed out; the tasks for such propulsion system are described. The modern classification of electric thrusters is given, in accordance of that one there are four classes, dissimilar due to a nature of processes that impart a kinetic energy to a propellant: electrothermal, electrostatic, pulsed and magnetoplasmodynamic. In order to illustrate an electric rocket thrusters sate of art, examples different classes electric rocket thrusters for modern spacecrafts are presented; the technical characteristics, such a thrust,
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27

Stude, Joan, Heinfried Aufmhoff, Hans Schlager, Markus Rapp, Frank Arnold, and Boris Strelnikov. "A novel rocket-borne ion mass spectrometer with large mass range: instrument description and first-flight results." Atmospheric Measurement Techniques 14, no. 2 (2021): 983–93. http://dx.doi.org/10.5194/amt-14-983-2021.

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Abstract. We present a novel rocket-borne ion mass spectrometer named ROMARA (ROcket-borne MAss spectrometer for Research in the Atmosphere) for measuring atmospheric positive and negative ions (atomic, molecular and cluster ions) and positively and negatively charged meteor smoke particles. Our ROMARA instrument has, compared to previous rocket-borne ion mass spectrometers, a markedly larger mass range of up to m/z 2000 and a larger sensitivity, particularly for meteor smoke particle detection. The major objectives of this first ROMARA flight included the following: a functional test of the R
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Hart, Grant W., and Kent L. Gee. "Assessing the impact of ground reflection on measurement of the overall sound power level and acoustic radiation efficiency of rocket launches." Journal of the Acoustical Society of America 152, no. 4 (2022): A256. http://dx.doi.org/10.1121/10.0016194.

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Determining the sound power levels of a rocket is the first step in characterizing its radiation efficiency. Because the sound radiation from a launch vehicle is anisotropic, well-calibrated ground measurement stations are used, along with trajectory data, to obtain sound power. Historically, the effect of ground reflections appears to largely have been neglected in the literature, despite the potential to inflate OAPWLs and therefore radiation efficiency. This study investigates the likely effect of a finite-impedance ground on spectra, overall sound pressure levels, and power levels. The sin
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Man’ko, Tamara Antonovna, and Kristina Viktorovna Коzis. "THE ISSUES OF CHEMISTRY AND TECHNOLOGIES OF RESIN MIXTURES FABRICATION FOR INTERNAL HEAT-PROTECTIVE COATING OF ROCKET SOLID FUEL ENGINE." Journal of Rocket-Space Technology 27, no. 4 (2019): 13–20. http://dx.doi.org/10.15421/451903.

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One of specific features of rocket engineering – is the high rate of sophistication and renewal of structures due to constantly growing operational and technical specifications imposed to them. Every generation of rocket and space products features a new complex of design and processing parameters and new materials possessing higher properties. It is impossible to resolve the entire scope of design and processing tasks in course of development, creation and operation of spacecraft without extend development and infusion of new materials which possess a number of required characteristics impose
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He, Qi. "An analysis of the art of gardening in Dongguan's Ke Garden and its inspiration." Highlights in Art and Design 1, no. 3 (2022): 61–64. http://dx.doi.org/10.54097/hiaad.v1i3.2961.

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Dongguan gives many people the impression that it is a manufacturing kingdom with factories all over the city. In fact, Dongguan is not a cultural desert in the eyes of many people; it is also an ancient city with a deep literary and artistic heritage and accumulation. Especially in the heart of the city lies a small but exquisitely designed garden of the Qing Dynasty, the Ke Garden. It can be described as a unique artisanal and Auxiliary side. The four famous gardens of Guangdong (Qinghui Garden in Shunde, Liang Yuan in Foshan, Ke Yuan in Dongguan and Yu Yin Shan Fang in Panyu) are representa
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KIM, Sa-Ra. "What Is the Reason for Learning Art?: Changes of Learner’s Recognition on Art through Art Expression Teaching." Korean Association For Learner-Centered Curriculum And Instruction 22, no. 15 (2022): 575–90. http://dx.doi.org/10.22251/jlcci.2022.22.15.575.

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Objectives This study started from the fact that confinement in the formalism of art expression cannot persuade students to answer the question of ‘What is the reason for learning art?’. Hence, the purpose of this study is to clarify whether learner’s recognition on art can be changed through the case on teaching art expression.
 Methods This study is done for the objects of the three 6th graders with insufficient confidence in practical skills in art. The researcher planned and practiced art expression class for one 6th grader and analyzed the study result by focusing on the student’s wo
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Pop, Virgiliu. "Rockets, Astronauts, and Shrines: Representations of Spaceflight in Sacred Visual Art and Architecture." Astropolitics 11, no. 1-2 (2013): 79–99. http://dx.doi.org/10.1080/14777622.2013.803215.

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Komurasaki, Kimiya, and Kuniyoshi Tabata. "Development of a Novel Launch System Microwave Rocket Powered by Millimeter-Wave Discharge." International Journal of Aerospace Engineering 2018 (December 30, 2018): 1–9. http://dx.doi.org/10.1155/2018/9247429.

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This paper presents the state of art of Microwave Rocket development and related researches on atmospheric discharge in a high-power millimeter-wave beam. Its operational mechanisms, thruster design, history of development, and flight path and cost analyses are introduced along with millimeter-wave discharge observations and numerical simulations. A thruster model of 126 g weight with no on-board propellant was launched to 1.2 m altitude using a 1 MW class gyrotron. A flight analysis that shows 77% cost reduction is possible using Microwave Rocket as the first stage of H-IIB heavy. A millimete
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Eberhart, M., S. Löhle, A. Steinbeck, T. Binder, and S. Fasoulas. "Measurement of atomic oxygen in the middle atmosphere using solid electrolyte sensors and catalytic probes." Atmospheric Measurement Techniques 8, no. 9 (2015): 3701–14. http://dx.doi.org/10.5194/amt-8-3701-2015.

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Abstract. The middle- and upper-atmospheric energy budget is largely dominated by reactions involving atomic oxygen (O). Modeling of these processes requires detailed knowledge about the distribution of this oxygen species. Understanding the mutual contributions of atomic oxygen and wave motions to the atmospheric heating is the main goal of the rocket project WADIS (WAve propagation and DISsipation in the middle atmosphere). It includes, amongst others, our instruments for the measurement of atomic oxygen that have both been developed with the aim of resolving density variations on small vert
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Sirieys, Elwyn, Chloe Gentgen, Julia Milton, and Olivier de Weck. "Space sustainability isn’t just about space debris: On the atmospheric impact of space launches." MIT Science Policy Review 3 (August 29, 2022): 143–51. http://dx.doi.org/10.38105/spr.whfig18hta.

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Throughout their life cycle, space launch vehicles impact their local and global environments on Earth and in space. Given the space industry’s projected growth, recent literature suggests that the atmospheric consequences of these activities are understudied and insufficiently addressed. Rockets uniquely emit combustion gases and particles into distinct layers of the atmosphere, inducing effects that include perturbations of ozone chemistry and of Earth’s energy balance through radiative forcing. International environmental regulations do not presently address rocket emissions and only scarce
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Amado, Javier Carlos Quagliano, Pablo Germán Ross, Natália Beck Sanches, Juliano Ribeiro Aguiar Pinto, and Jorge Carlos Narciso Dutra. "Evaluation of elastomeric heat shielding materials as insulators for solid propellant rocket motors: A short review." Open Chemistry 18, no. 1 (2020): 1452–67. http://dx.doi.org/10.1515/chem-2020-0182.

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AbstractThis review addresses a comparison, based on the literature, among nitrile rubber (NBR), ethylene-propylene-diene-monomer rubber (EPDM), and polyurethane (PU) elastomeric heat shielding materials (EHSM). Currently, these are utilized for the insulation of rocket engines to prevent catastrophic breakdown if combustion gases from propellant reaches the motor case. The objective of this review is to evaluate the performance of PU–EHSM, NBR–EHSM, and EPDM–EHSM as insulators, the latter being the current state of the art in solid rocket motor (SRM) internal insulation. From our review, PU–E
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QIAO, Xiting. "Re-imagining the History of British Abolition: The New Historical Consciousness in Winsome Pinnock's Rockets and Blue Lights." Theatre Academy 2, no. 1 (2024): 15–31. https://doi.org/10.5281/zenodo.10829667.

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Examining Winsome Pinnock’s Rockets and Blue Lights through a new-historical lens, this study aims to shed light on the theatrical intervention in the historical narrative of the British abolition, and to evaluate Pinnock's contribution to modern art and its interpretation through her attempt to highly fictionalize history. By constructing the protagonist J. M. W. Turner as an anti-hero, Pinnock places Turner back in a Victorian ethical context to question the arbitrary construction of Turner’s heroism by the complicity of discourses of art history and abolitionism. The juxtapositi
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Lin, Binbin, Hongliang Pan, Lei Shi, and Jinying Ye. "Effect of Primary Rocket Jet on Thermodynamic Cycle of RBCC in Ejector Mode." International Journal of Turbo & Jet-Engines 37, no. 1 (2020): 61–70. http://dx.doi.org/10.1515/tjj-2017-0013.

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AbstractThrust augmentation in ejector mode is important to improve engine performance so as to enable more propulsion applications of RBCC. Usually, the internal flow-path is configured mainly for combustion organization in ramjet and scramjet modes, thus the RBCC performance in ejector mode will mainly depend on the primary rocket operating parameters and jet expansion state. Considering such restrictions and requirements on the primary rocket, this paper studies the effects of the primary rocket jet on the thermodynamic cycle performance of ejector mode, in which incoming air is dominated b
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Gruen, Russell, and Ross Bailie. "Specialist clinics in remote Australian Aboriginal communities: where rock art meets rocket science." Journal of Health Services Research & Policy 9, no. 2_suppl (2004): 56–62. http://dx.doi.org/10.1258/1355819042349844.

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Igor, Trofimov, Boichenko Sergii, and Shamanskyi Sergii. "Analysis of rocket fuels and problems of their application on the example of Ukraine." TECHNOLOGY AUDIT AND PRODUCTION RESERVES 6, no. 1(56) (2020): 19–27. https://doi.org/10.15587/2706-5448.2020.218358.

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<em>The object of research is the problems of rocket fuel application, the state of art and prospects. These problems are characteristic of almost the entire range of brands of modern rocket fuels suitable for application. These are problems with the basic physic-chemical and operational properties, technical requirements for the quality of rocket fuel, problems with the functioning of the refueling infrastructure, as well as ensuring the purity of rocket fuels.</em> <em>Given the ban on the use of highly toxic poisonous rocket fuels based on nitric acid, there is a problem of replacing them w
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Крічлоу, К. В., О. В. Колосніченко, Т. В. Струмінська, Б. О. Процик та Б. В. Касс. "Виникнення стилів "байкер" і "рокер" у сучасній світовій моді". Art and Design, № 4 (15 лютого 2021): 123–35. http://dx.doi.org/10.30857/2617-0272.2020.4.10.

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Study of the prerequisites of the emergence of Bikers and Rockers archetypes and their influence on the formation of corresponding subcultures and the direction of independent world fashion styles. The work uses a historical analysis and a visual-analytical method based on illustrative publications to study the artistic and compositional features of rider's clothing. Based on the scientific works of K. Jung, the influence of the collective unconscious on the process of the emergence of "bikers" and "rockers" subcultures are determined. The prerequisites at the inception of these styles were co
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Pineau, Adrien, Henriette Trollvik, Herman Greaker, Sveinung Olsen, Yngve Eilertsen, and Ingrid Mann. "Simulations of the collection of mesospheric dust particles with a rocket instrument." Atmospheric Measurement Techniques 17, no. 12 (2024): 3843–61. http://dx.doi.org/10.5194/amt-17-3843-2024.

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Abstract. We investigate the collection of dust particles in the mesosphere with the MESS (MEteoric Smoke Sampler) instrument that is designed to fly on a sounding rocket. We assume that the ice particles that form in the polar mesosphere between 80 and 85 km altitude in summer contain meteoric smoke particles; and these should be collected with MESS. The instrument consists of a collection device with an opening and closure mechanism, as well as an attached conic funnel which increases the sampling area in comparison to the collection area. Dust particles are collected either directly after p
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Crompton, R. W., G. D. Dracoulis, B. R. Lewis, K. G. McCracken, and J. S. Williams. "John Henry Carver 1926 - 2004." Historical Records of Australian Science 22, no. 1 (2011): 53. http://dx.doi.org/10.1071/hr10015.

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John Henry Carver made distinguished contributions to national and international physics, not only through his research in nuclear physics, atomic and molecular physics, and planetary atmospheric physics, but also as a scientific administrator. His years as the Elder Professor of Physics at the University of Adelaide saw him enter the field of rocket-based atmospheric physics by forging strong links with the nearby Weapons Research Establishment through which he had access to rockets to fly equipment developed in his laboratory and, eventually, to launch a small satellite developed and built b
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Tigrini, Andrea, Rami Mobarak, Alessandro Mengarelli, et al. "Phasor-Based Myoelectric Synergy Features: A Fast Hand-Crafted Feature Extraction Scheme for Boosting Performance in Gait Phase Recognition." Sensors 24, no. 17 (2024): 5828. http://dx.doi.org/10.3390/s24175828.

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Gait phase recognition systems based on surface electromyographic signals (EMGs) are crucial for developing advanced myoelectric control schemes that enhance the interaction between humans and lower limb assistive devices. However, machine learning models used in this context, such as Linear Discriminant Analysis (LDA) and Support Vector Machine (SVM), typically experience performance degradation when modeling the gait cycle with more than just stance and swing phases. This study introduces a generalized phasor-based feature extraction approach (PHASOR) that captures spatial myoelectric featur
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Kim, Jeong Soo, Hun Jung, and Jong Hyun Kim. "State of the Art in the Development of Methane/Oxygen Liquid-bipropellant Rocket Engine." Journal of the Korean Society of Propulsion Engineers 17, no. 6 (2013): 120–30. http://dx.doi.org/10.6108/kspe.2013.17.6.120.

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., Almuzakkir, Muhammad ., and Adi Setiawan. "Performance Test of a Household Rocket Stoves Fired with Coconut Frond, Coconut Shell and Bamboo." International Journal of Research and Review 8, no. 1 (2021): 59–64. http://dx.doi.org/10.52403/ijrr.20210107.

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Fuel is something that is very important in everyday life. Almost every human being needs fuel to meet their needs and support their activities, for example cooking in household needs. Currently, fossil fuels or fuel oil (BBM) are still widely used to meet demand, however, it should be noted that fossil fuels or fuel oil (BBM) are non-renewable natural resources. The biomass rocket stove is one of the modern stove innovations that uses biomass energy as the main energy source. Rocket stoves are designed to increase fuel efficiency with thermal efficiency, a combination of the increased combust
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Waesche, R. H. Woodward, William H. Sargent, and J. F. Marchman. "Space Shuttle solid rocket motor aft-end internal flows." Journal of Propulsion and Power 5, no. 6 (1989): 650–56. http://dx.doi.org/10.2514/3.23202.

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Mason, B. P., and C. M. Roland. "SOLID PROPELLANTS." Rubber Chemistry and Technology 92, no. 1 (2019): 1–24. http://dx.doi.org/10.5254/rct.19.80456.

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ABSTRACT Solid propellants are energetic materials used to launch and propel rockets and missiles. Although their history dates to the use of black powder more than two millennia ago, greater performance demands and the need for “insensitive munitions” that are resistant to accidental ignition have driven much research and development over the past half-century. The focus of this review is the material aspects of propellants, rather than their performance, with an emphasis on the polymers that serve as binders for oxidizer particles and as fuel for composite propellants. The prevalent modern b
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Sharpe, Kenan Behzat. "Poetry, Rock ’n’ Roll, and Cinema in Turkey’s 1960s." Turkish Historical Review 12, no. 2-3 (2021): 353–78. http://dx.doi.org/10.1163/18775462-bja10028.

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Abstract Using developments in poetry, music, and cinema as case studies, this article examines the relationship between left-wing politics and cultural production during the long 1960s in Turkey. Intellectual and artistic pursuits flourished alongside trade unionism, student activism, peasant organizing, guerrilla movements. This article explores the convergences between militants and artists, arguing for the centrality of culture in the social movements of the period. It focuses on three revealing debates: between the modernist İkinci Yeni poets and young socialist poets, between left-wing p
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Eberhart, Martin, Stefan Löhle, Boris Strelnikov, et al. "Atomic oxygen number densities in the mesosphere–lower thermosphere region measured by solid electrolyte sensors on WADIS-2." Atmospheric Measurement Techniques 12, no. 4 (2019): 2445–61. http://dx.doi.org/10.5194/amt-12-2445-2019.

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Abstract. Absolute profiles of atomic oxygen number densities with high vertical resolution have been determined in the mesosphere–lower thermosphere (MLT) region from in situ measurements by several rocket-borne solid electrolyte sensors. The amperometric sensors were operated in both controlled and uncontrolled modes and with various orientations on the foredeck and aft deck of the payload. Calibration was based on mass spectrometry in a molecular beam containing atomic oxygen produced in a microwave discharge. The sensor signal is proportional to the number flux onto the electrodes, and the
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