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Journal articles on the topic 'Hydrogen peroxide rockets'

Author: Grafiati

Published: 4 June 2021

Last updated: 11 February 2022

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1

Okninski, Adam, Pawel Surmacz, Bartosz Bartkowiak, et al. "Development of Green Storable Hybrid Rocket Propulsion Technology Using 98% Hydrogen Peroxide as Oxidizer." Aerospace 8, no. 9 (2021): 234. http://dx.doi.org/10.3390/aerospace8090234.

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This paper presents the development of indigenous hybrid rocket technology, using 98% hydrogen peroxide as an oxidizer. Consecutive steps are presented, which started with interest in hydrogen peroxide and the development of technology to obtain High Test Peroxide, finally allowing concentrations of up to 99.99% to be obtained in-house. Hydrogen peroxide of 98% concentration (mass-wise) was selected as the workhorse for further space propulsion and space transportation developments. Over the course nearly 10 years of the technology’s evolution, the Lukasiewicz Research Network—Institute of Avi

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2

Pasini, A., L. Torre, L. Romeo, A. Cervone, and L. d’Agostino. "Performance Characterization of Pellet Catalytic Beds for Hydrogen Peroxide Monopropellant Rockets." Journal of Propulsion and Power 27, no. 2 (2011): 428–36. http://dx.doi.org/10.2514/1.b34000.

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3

Bonifacio, S., G. Festa, and A. Russo Sorge. "Novel Structured Catalysts for Hydrogen Peroxide Decomposition in Monopropellant and Hybrid Rockets." Journal of Propulsion and Power 29, no. 5 (2013): 1130–37. http://dx.doi.org/10.2514/1.b34864.

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4

Lee, Eunkwang, Hongjae Kang, and Sejin Kwon. "Demonstration of Thrust Vector Control by Hydrogen Peroxide Injection in Hybrid Rockets." Journal of Propulsion and Power 35, no. 1 (2019): 109–14. http://dx.doi.org/10.2514/1.b37074.

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5

Farbar, E., J. Louwers, and T. Kaya. "Investigation of Metallized and Nonmetallized Hydroxyl Terminated Polybutadiene/Hydrogen Peroxide Hybrid Rockets." Journal of Propulsion and Power 23, no. 2 (2007): 476–86. http://dx.doi.org/10.2514/1.22091.

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6

Yun, Yongtae, Jeongmoo Huh, and Sejin Kwon. "Port diameter design of multiport solid fuel in hydrogen peroxide hybrid rockets." Aerospace Science and Technology 110 (March 2021): 106485. http://dx.doi.org/10.1016/j.ast.2020.106485.

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7

Ahn, Byeonguk, Jeongmoo Huh, Vikas Khandu Bhosale, and Sejin Kwon. "Three-Dimensionally Printed Polylactic Acid as Solid Fuel for Hydrogen Peroxide Hybrid Rockets." Journal of Propulsion and Power 37, no. 1 (2021): 171–75. http://dx.doi.org/10.2514/1.b37957.

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8

John, Jerin, Purushothaman Nandagopalan, Seung Wook Baek, and Sung June Cho. "Hypergolic ignition delay studies of solidified ethanol fuel with hydrogen peroxide for hybrid rockets." Combustion and Flame 212 (February 2020): 205–15. http://dx.doi.org/10.1016/j.combustflame.2019.10.029.

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9

Zhang, Yue, and Xuan J. Wang. "The Preparation of Graphite Oxide Controlled by Optimum Oxidation Potential with any Rejected Nitro-Oxidizer." Nano 14, no. 02 (2019): 1950018. http://dx.doi.org/10.1142/s1793292019500188.

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Nitro-oxidizers (nitric acid-27S, nitrogen tetroxide and mixed nitrogen oxide) are common liquid oxidants widely used in liquid rockets and missile weapons. How to deal with large quantities of scrapped nitro-oxidizers is a complex, costly and dangerous project. We pretreated it with hydrogen peroxide (H2O[Formula: see text] and converted the active oxidant component of nitro-oxidizers into nitric acid, which can be used as oxidant source to prepare graphite oxide from natural graphite. The comprehensive oxidation ability of the reaction system can be effectively controlled by adding different

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10

Tsujikado, Nobuo, and Atsushi Ishihara. "90% HYDROGEN PEROXIDE/POLYETHYLENE HYBRID ROCKET." International Journal of Energetic Materials and Chemical Propulsion 7, no. 4 (2008): 263–80. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v7.i4.10.

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11

Al – Daraji, Hazim J. "Effect of dietary supplementation with rocket salad (Eruca sativa) seeds powder on certain seminal plasma traits of Hy – line laying breeder roosters subjected to oxidative stress induced by hydrogen peroxide." Iraqi Journal of Veterinary Medicine 36, no. 0A (2012): 62–69. http://dx.doi.org/10.30539/iraqijvm.v36i0a.356.

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This study was conducted to evaluate the effect of adding different levels of rocket salad seeds powder to the diet on seminal plasma traits of roosters subjected to oxidative stress induced by hydrogen peroxide. A total of 60 Hy – line laying breeder roosters 57 weeks old were used in this study. Roosters were randomly distributed into 5 treatments with 3 replicates each. Each replicate constituted of 4 roosters (12 roosters for each treatment). Experimental treatments were as following: T1: Males fed control diet and normal water, T2: Males fed diet supplemented with 3 gm rocket salad powder

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12

PELIN, George, Cornel STOICA, Cristina Elisabeta PELIN, and Raluca BALASA. "High concentration hydrogen peroxide for rocket fuel applications." INCAS BULLETIN 12, no. 3 (2020): 151–57. http://dx.doi.org/10.13111/2066-8201.2020.12.3.12.

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This paper presents the experimental study of the distillation of hydrogen peroxide to increase the concentration of the solution, in order to use it as rocket fuel in space applications. The process of obtaining the desired concentration required for the operation of the wind tunnel model rocket engine was obtained using the vacuum distillation method. The process consists in removing a calculated value of the water content from the hydrogen peroxide solution with a concentration of 35%, thus increasing its concentration up to the value of 90%. The key factors that contribute in obtaining the

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13

LEE, Yang-Suk, and Jun Hwan JANG. "The design and performance on 200N-class bipropellant rocket engine using decomposed H2O2 and Kerosene." INCAS BULLETIN 11, no. 3 (2019): 99–110. http://dx.doi.org/10.13111/2066-8201.2019.11.3.9.

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Mono-propellant thrusters are widely utilized in satellites and space launchers. In many cases, they are using hydrazine as a propellant. However, hydrazine has high toxicity and high risks in using for launch campaign. Recently, low-toxic (green) propellant is being highlighted as a replacement for hydrazine. In this paper, 200N bi-propellant engine using hydrogen peroxide/kerosene was designed/manufactured, and the spray or atomization characteristic and inflation pressure were determined by cold flow test, and combustion and pulse tests in a single cycle same as previous methods were conduc

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14

Guseinov, Sh L., S. G. Fedorov, V. A. Kosykh, and P. A. Storozhenko. "Hydrogen Peroxide Decomposition Catalysts Used in Rocket Engines." Russian Journal of Applied Chemistry 93, no. 4 (2020): 467–87. http://dx.doi.org/10.1134/s1070427220040011.

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15

Ahn, Byeonguk, Hongjae Kang, Eunkwang Lee, Yongtae Yun, and Sejin Kwon. "Design of Multiport Grain with Hydrogen Peroxide Hybrid Rocket." Journal of Propulsion and Power 34, no. 5 (2018): 1189–97. http://dx.doi.org/10.2514/1.b36949.

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16

Huh, Jeongmoo, Botchu V. S. Jyoti, Yongtae Yun, M. N. Shoaib, and Sejin Kwon. "Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster." International Journal of Aerospace Engineering 2018 (December 30, 2018): 1–14. http://dx.doi.org/10.1155/2018/5630587.

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In regard to propulsion system applications, the stability of liquid propellants in long-term storage is of increasing importance, and this had led to a greater interest in gelation technology. As part of a preliminary test to determine the feasibility of using a gel propellant in a rocket with a catalyst bed, a hybrid rocket with a catalyst reactor using a gel propellant as an oxidizer was tested for the first time in this study. Experiments were conducted with two different oxidizers: one with liquid phase hydrogen peroxide and the other with gel phase hydrogen peroxide, as well as high-dens

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17

Wernimont, E. J., and S. D. Heister. "Combustion Experiments in Hydrogen Peroxide/Polyethylene Hybrid Rocket with Catalytic Ignition." Journal of Propulsion and Power 16, no. 2 (2000): 318–26. http://dx.doi.org/10.2514/2.5571.

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18

Ventura, M. C., and S. D. Heister. "Hydrogen peroxide as an alternate oxidizer for a hybrid rocket booster." Journal of Propulsion and Power 11, no. 3 (1995): 562–65. http://dx.doi.org/10.2514/3.23878.

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19

Rusek, John J. "New decomposition catalysts and characterization techniques for rocket-grade hydrogen peroxide." Journal of Propulsion and Power 12, no. 3 (1996): 574–79. http://dx.doi.org/10.2514/3.24071.

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20

Kozhevnikov, A., M. Semushina, E. Podrukhina, and D. Kosyakov. "Modification of Hydrolysis Lignin by Hydrogen Peroxide to Obtain an Effective Adsorbent of Highly Toxic Rocket Fuel." Eurasian Chemico-Technological Journal 19, no. 2 (2017): 155. http://dx.doi.org/10.18321/ectj646.

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Lignin, a large scale by-product of papermaking and bioethanol production, is applied now in various fields. One of the main areas of use is in the development of different adsorbents, including those intended for detoxification of the spills of 1,1-dimethylhydrazine-based rocket fuel. The present work has shown the possibility of oxidative modification of hydrolytic lignin by hydrogen peroxide to improve the efficiency of the adsorbent. The change in functional composition of the modified adsorbent was studied by IR and NMR spectroscopy. It was shown that the oxidative treatment led to an inc

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21

Whitmore, Stephen A., Christopher J. Martinez, and Daniel P. Merkley. "Catalyst development for an arc-ignited hydrogen peroxide/ABS hybrid rocket system." Aeronautics and Aerospace Open Access Journal 2, no. 6 (2018): 356–88. http://dx.doi.org/10.15406/aaoaj.2018.02.00069.

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22

Maia, Fernanda F., Luis G. F. Pereira, Leonardo H. Gouvea, Fernando S. Costa, and Ricardo Vieira. "CoMn-Based Oxides as Bulk Catalyst for Rocket-Grade Hydrogen Peroxide Decomposition." Journal of Propulsion and Power 30, no. 2 (2014): 309–13. http://dx.doi.org/10.2514/1.b34996.

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23

Ferroni Pereira, Luís Gustavo, Leandro José Maschio, Emmanuel Péres de Araújo, Leonardo Henrique Gouvêa, and Ricardo Vieira. "CoMn‐Spinel Oxides as Supported Catalyst for Rocket‐Grade Hydrogen Peroxide Decomposition." Propellants, Explosives, Pyrotechnics 45, no. 10 (2020): 1627–33. http://dx.doi.org/10.1002/prep.202000020.

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24

POURPOINT, TIMOTHÉE L., and WILLIAM E. ANDERSON. "HYPERGOLIC REACTION MECHANISMS OF CATALYTICALLY PROMOTED FUELS WITH ROCKET GRADE HYDROGEN PEROXIDE." Combustion Science and Technology 179, no. 10 (2007): 2107–33. http://dx.doi.org/10.1080/00102200701386149.

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25

Romantsova, O. V., and V. B. Ulybin. "Safety issues of high-concentrated hydrogen peroxide production used as rocket propellant." Acta Astronautica 109 (April 2015): 231–34. http://dx.doi.org/10.1016/j.actaastro.2014.10.022.

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26

Zhao, Bo, Nanjia Yu, Yufei Liu, Peng Zeng, and Jue Wang. "Unsteady simulation and experimental study of hydrogen peroxide throttleable catalyst hybrid rocket motor." Aerospace Science and Technology 76 (May 2018): 27–36. http://dx.doi.org/10.1016/j.ast.2018.02.008.

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27

Whitmore, Stephen A., Isaac W. Armstrong, Mark C. Heiner, and Christopher J. Martinez. "High-performing hydrogen peroxide hybrid rocket with 3-D printed and extruded ABS fuel." Aeronautics and Aerospace Open Access Journal 2, no. 6 (2018): 334–54. http://dx.doi.org/10.15406/aaoaj.2018.02.00068.

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28

Paulsen, Riley T., and Dmitri S. Kilin. "Silver Nanoparticles for Catalysis of Hydrogen Peroxide Decomposition: Atomistic Modeling." MRS Proceedings 1787 (2015): 21–25. http://dx.doi.org/10.1557/opl.2015.731.

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ABSTRACTThe interest in adopting hydrogen peroxide (H2O2) rocket propulsion systems has rekindled because H2O2 is more environmentally friendly than alternative propellants, has a high density to maximize the oxidizer-to-fuel ratio, and is able to be stored non-cryogenically. Simulations utilizing ab initio molecular dynamics have been generated to analyze the decomposition of H2O2 on the surface of a silver (Ag) metal cluster. The electronic structure for an atomic model of gaseous H2O2 molecules in the vicinity of an Ag13 cluster – one central Ag atom coordinated by the remaining twelve Ag a

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29

Towner, Tyler W., and Donald G. Plumlee. "Design and Fabrication of LTCC Catalyst Chambers." Additional Conferences (Device Packaging, HiTEC, HiTEN, and CICMT) 2011, CICMT (2011): 000037–42. http://dx.doi.org/10.4071/cicmt-2011-ta15.

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The reduction in satellite size and mass presents the need to develop a proportionally smaller propulsion system for orbital station keeping. A liquid, monopropellant micropropulsion device made from Low Temperature Co-Fired Ceramics (LTCC) has been developed at Boise State University. This robust, simple design uses an embedded silver catalyst chamber to decompose a rocket-grade hydrogen peroxide monopropellant into a hot gas, which is then expelled out through a nozzle to generate thrust. Using LTCC eliminates the planar geometry fabrication constraint commonly found in silicon MEMS processi

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30

Yun, Yongtae, Jeongmoo Huh, Youngil Kim, Seonuk Heo, Hyuntak Kim, and Sejin Kwon. "Scale-Up Validation of Hydrogen Peroxide/High-Density Polyethylene Hybrid Rocket with Multiport Solid Fuel." Journal of Spacecraft and Rockets 58, no. 2 (2021): 552–65. http://dx.doi.org/10.2514/1.a34707.

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31

Cai, Guobiao, Chengen Li, and Hui Tian. "Numerical and experimental analysis of heat transfer in injector plate of hydrogen peroxide hybrid rocket motor." Acta Astronautica 128 (November 2016): 286–94. http://dx.doi.org/10.1016/j.actaastro.2016.05.041.

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32

LEPAUS, Bárbara Morandi, Jéssica Souza ROCHA, and Jackline Freitas Brilhante de SÃO JOSÉ. "Organic acids and hydrogen peroxide can replace chlorinated compounds as sanitizers on strawberries, cucumbers and rocket leaves." Food Science and Technology 40, suppl 1 (2020): 242–49. http://dx.doi.org/10.1590/fst.09519.

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33

Chen, Song, Jian Li, Lei Wei, et al. "Comparative effects of rocket-grade hydrogen peroxide solution on POM and UHMWPE: aging behaviors and tribological properties." Colloid and Polymer Science 296, no. 6 (2018): 1087–96. http://dx.doi.org/10.1007/s00396-018-4322-y.

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34

Li, Sen, Yifei Ge, Xiaolin Wei, and Teng Li. "Mixing and combustion modeling of hydrogen peroxide/kerosene shear-coaxial jet flame in lab-scale rocket engine." Aerospace Science and Technology 56 (September 2016): 148–54. http://dx.doi.org/10.1016/j.ast.2016.07.008.

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35

Zeff, Jack D., and Jerome T. Barich. "UV/Oxidation of Organic Contaminants in Ground, Waste and Leachate Waters." Water Quality Research Journal 27, no. 1 (1992): 139–50. http://dx.doi.org/10.2166/wqrj.1992.008.

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Abstract Over the past four years, Ultrox International has demonstrated the efficacy of ultraviolet light-enhanced oxidation at industrial, Department of Defense and Superfund sites. Waters containing halogenated solvents such as trichloroethylene, perchloroethylene and other halogenated compounds have been successfully treated with UV/ozone or UV/hydrogen peroxide or UV with ozone and peroxide. Other contaminants such as benzene, toluene, xylene, hydrazines, phenols, chlorophenols, dioxanes, PCBs and pesticides in wastewaters and groundwaters have also been reduced to acceptable discharge st

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36

Maschio, Leandro José, Luis Gustavo Ferroni Pereira, William Müller Meyer, Rodrigo Intini Marques, and Ricardo Vieira. "A DOE STUDY ON THE HYPERGOLICITY OF HYDROGEN PEROXIDE WITH A ROCKET LIQUID FUEL BASED ON MONOETHANOLAMINE AND ETHANOL." International Journal of Energetic Materials and Chemical Propulsion 17, no. 2 (2018): 137–45. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.2018029025.

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37

Ha, Seong-Up, Seon-Mi Lee, In-Sang Moon, and Soo-Yong Lee. "Numerical Simulations on Combustion Considering Propellant Droplet Atomization and Evaporation of 500 N Class Hydrogen Peroxide / Kerosene Rocket Engine." Journal of the Korean Society for Aeronautical & Space Sciences 40, no. 10 (2012): 862–71. http://dx.doi.org/10.5139/jksas.2012.40.10.862.

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38

Li, Huixin, Liang Ye, Xiaolin Wei, Teng Li, and Sen Li. "The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine." Aerospace Science and Technology 70 (November 2017): 636–43. http://dx.doi.org/10.1016/j.ast.2017.09.003.

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39

Pacholczak, Andrzej, Małgorzata Zajączkowska, and Karolina Nowakowska. "The Effect of Brassinosteroids on Rootting of Stem Cuttings in Two Barberry (Berberis thunbergii L.) Cultivars." Agronomy 11, no. 4 (2021): 699. http://dx.doi.org/10.3390/agronomy11040699.

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Brassinosteroids are a group of over seventy steroid compounds whose discovery in lower and higher plant organisms created new possibilities of plant growth control. The aim of the work was to evaluate the effect of two brassinosteroids: brassinolide (BL) and 24-epibrassinolide (24epiBL) as compared to the auxin rooting enhancer indole-3-butyric acid (IBA), on the rooting of stem cuttings in two Thunberg’s barberry cultivars ‘Maria’ and ‘Red Rocket’. The cuttings were sprayed with water solutions of growth regulators: IBA (200 mg·L−1), 0.05% BL or 24epiBL, as well as with a combination of each

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40

Vorobiev, A. G., I. N. Borovik, and Song-Up Ha. "Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling." VESTNIK of the Samara State Aerospace University, no. 1(43) (July 30, 2014): 30. http://dx.doi.org/10.18287/1998-6629-2014-0-1(43)-30-40.

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41

Ariyanti, Dhita, and Muhammad Syaifuddin. "Au Extraction from Mineral Rocks with Aeration-Cyanidation Hydrometallurgy and Comparative Study of Its Effectiveness in Various Methods and Solvents." JKPK (Jurnal Kimia dan Pendidikan Kimia) 4, no. 2 (2019): 115. http://dx.doi.org/10.20961/jkpk.v4i2.29020.

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<p>Indonesia is a country with abundant mining potential, one of it is gold (Au) which has a high economic value. Separation of gold metal from mineral rock consists of several methods, such as extraction, hydrometallurgy, and membrane emulsifier technology. These three methods produce different effectiveness of percentage recovery (%recovery), depend on the optimum conditions of each method and type of solvent. This study aims to separate the gold metal from mineral rocks through the hydrometallurgical method with an aeration-cyanidation solvent combination. Hidrometallurgy method is li

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42

Wei, S. S., M. C. Lee, Y. H. Chien, T. H. Chou, and J. S. Wu. "Experimental investigation of the effect of nozzle throat diameter on the performance of a hybrid rocket motor with swirling injection of high-concentration hydrogen peroxide." Acta Astronautica 164 (November 2019): 334–44. http://dx.doi.org/10.1016/j.actaastro.2019.07.020.

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43

Xylia, Panayiota, George Botsaris, Panagiotis Skandamis, and Nikolaos Tzortzakis. "Expiration Date of Ready-to-Eat Salads: Effects on Microbial Load and Biochemical Attributes." Foods 10, no. 5 (2021): 941. http://dx.doi.org/10.3390/foods10050941.

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When minimally processed vegetables reach their expiration date, expose an increased microbial load. This includes mainly spoilage microorganisms but also foodborne pathogens, thus affecting the quality and safety of highly consumed ready-to-eat salads. A total of 144 ready-to-eat salads from the Cypriot market were analyzed in an attempt to determine the effects of the expiration date on the microbial load and plant metabolic variables of the salads. Possible correlations between them were also investigated for the first time. Furthermore, the impacts of the season (winter, summer), salad pro

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44

Andriievskyi, M. V., and Yu O. Mitikov. "Influence of propellant leakage from pump area into turbine area on turbo-pump operation stability." Kosmìčna nauka ì tehnologìâ 27, no. 1 (2021): 97–102. http://dx.doi.org/10.15407/knit2021.01.097.

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There is an increasing trend to liquid-propellant rocket engines which run on eco-friendly storable propellant. This trend is mostly dictated by the refusal to use traditional toxic storable propellant in many countries. The most widespread eco-friendly storable propellant is hydrogen peroxide with kerosene. Though, this propellant has a lower specific impulse in comparison with traditional liquid oxygen with kerosene. To compensate the loss of specific impulse, there is a reason to design a staged combustion engine. Evidently, the turbopump is the most complicated system in the staged combust

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45

Nosseir, Ahmed E. S., Angelo Cervone, and Angelo Pasini. "Review of State-of-the-Art Green Monopropellants: For Propulsion Systems Analysts and Designers." Aerospace 8, no. 1 (2021): 20. http://dx.doi.org/10.3390/aerospace8010020.

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Current research trends have advanced the use of “green propellants” on a wide scale for spacecraft in various space missions; mainly for environmental sustainability and safety concerns. Small satellites, particularly micro and nanosatellites, evolved from passive planetary-orbiting to being able to perform active orbital operations that may require high-thrust impulsive capabilities. Thus, onboard primary and auxiliary propulsion systems capable of performing such orbital operations are required. Novelty in primary propulsion systems design calls for specific attention to miniaturization, wh

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46

Hussain, Affan. "Using Pyrolyzed Plastic as an Alternative Fuel Source of Rockets & Hydrogen Peroxide as an Oxidizer." SSRN Electronic Journal, 2021. http://dx.doi.org/10.2139/ssrn.3797779.

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47

"Toxicity of rocket fuels: comparison of hydrogen peroxide with current propellants." Fuel and Energy Abstracts 43, no. 1 (2002): 18. http://dx.doi.org/10.1016/s0140-6701(02)80174-6.

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48

"The Past and Future Perspectives of Hydrogen Peroxide as Rocket Propellants." Journal of the Korean Society for Aeronautical Space Science 37, no. 7 (2009): 717–28. http://dx.doi.org/10.5139/jksas.2009.37.7.717.

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49

Yun, Yongtae, Kyu-seop Kim, Vikas Khandu Bhosale, and Sejin Kwon. "Effect of Fuel Activation Energy on Ignition of Hydrogen Peroxide Hybrid Rocket." Journal of Spacecraft and Rockets, August 2, 2021, 1–5. http://dx.doi.org/10.2514/1.a35083.

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50

Wan Ali, Wan Khairuddin, Kiang Long Ang, and Mohammad Nazri Mohd. Jaafar. "Experimental Solid and Liquid Propellant Rocket Development in Universiti Teknologi Malaysia : 1992-2011." Jurnal Teknologi 73, no. 1 (2015). http://dx.doi.org/10.11113/jt.v73.3378.

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This paper reports on the research and development activities related to the experimental solid and liquid propellant rocket in Universiti Teknologi Malaysia (UTM) from year 1992 to 2011. A total of 41 closed access academic theses and project papers from UTM library archive were exclusively selected for this review work. Some of these theses and papers originally written in Malay language were translated into English language in this paper for better understanding of the research community. This paper gives a historical insight on the apparatus and methodology designed for educational researc

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