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Relevant bibliographies by topics / Hypergolic propellant

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Academic literature on the topic 'Hypergolic propellant'

Author: Grafiati

Published: 4 June 2021

Last updated: 7 February 2022

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Journal articles on the topic "Hypergolic propellant"

1

Davis, Stephen M., and Nadir Yilmaz. "Advances in Hypergolic Propellants: Ignition, Hydrazine, and Hydrogen Peroxide Research." Advances in Aerospace Engineering 2014 (September 15, 2014): 1–9. http://dx.doi.org/10.1155/2014/729313.

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A review of the literature pertaining to hypergolic fuel systems, particularly using hydrazine or its derivatives and hydrogen peroxide, has been conducted. It has been shown that a large effort has been made towards minimizing the risks involved with the use of a toxic propellant such as the hydrazine. Substitution of hydrazines for nontoxic propellant formulations such as the use of high purity hydrogen peroxide with various types of fuels is one of the major areas of study for future hypergolic propellants. A series of criteria for future hypergolic propellants has been recommended, includi

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2

Yuan, Wen-Li, Lei Zhang, Guo-Hong Tao, et al. "Designing high-performance hypergolic propellants based on materials genome." Science Advances 6, no. 49 (2020): eabb1899. http://dx.doi.org/10.1126/sciadv.abb1899.

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A new generation of rocket propellants for deep space exploration, ionic liquid propellants, with long endurance and high stability, is attracting more and more attention. However, a major defect of ionic liquid propellants that restricts their application is the inadequate hypergolic reactivity between the fuel and the oxidant, and this defect results in local burnout and accidental explosions during the launch process. We propose a visualization model to show the features of structure, density, thermal stability, and hypergolic activity for estimating propellant performances and their applic

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Mayer, Alfons, and Wolter Wieling. "Green Propulsion Research at TNO the Netherlands." Transactions on Aerospace Research 2018, no. 4 (2018): 1–24. http://dx.doi.org/10.2478/tar-2018-0026.

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Abstract This paper describes the recent theoretical and experimental research by the Netherlands Organisation for Applied Scientific Research (TNO) into green replacements for hydrazine, hydrazine derivatives and nitrogen tetroxide, as propellants for in-space propulsion. The goal of the study was to identify propellants that are capable of outperforming the current propellants for space propulsion and are significantly less hazardous for humans and the environment. Two types of propellants were investigated, being monopropellants and bipropellants. The first section of the paper discusses th

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Davis, Stephen M., and Nadir Yilmaz. "Thermochemical Analysis of Hypergolic Propellants Based on Triethylaluminum/Nitrous Oxide." International Journal of Aerospace Engineering 2014 (2014): 1–5. http://dx.doi.org/10.1155/2014/269836.

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The vacuum specific impulse, density vacuum specific impulse, and solid exhaust products were examined for several propellant formulations based on the pyrophoric material triethylaluminum (TEA) using CEA thermodynamics code. Evaluation of TEA neat and mixed with hydrocarbon fuels with LOX, N2O, N2O4, liquefied air, and HNO3were performed at stoichiometry. The vacuum specific impulse of neat TEA with N2O is comparable to that of nitric acid with the same, but the N2O formulation will produce slightly less solid products during combustion. Additionally, N2O-TEA propellants have vacuum specific

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MATSUNO, Shinsuke, Hiroyasu SAITOH, Fumiteru AKAMATSU, and Masashi KATSUKI. "Spray Characteristics of Hypergolic Propellant for Bi-propellant Thrusters." Proceedings of the Thermal Engineering Conference 2003 (2003): 503–4. http://dx.doi.org/10.1299/jsmeted.2003.503.

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Schwertz, Hansjrg, Lisa A. Roth, and Daniel Woodard. "Propellant Off-Gassing and Implications for Triage and Rescue." Aerospace Medicine and Human Performance 91, no. 12 (2020): 956–61. http://dx.doi.org/10.3357/amhp.5637.2020.

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INTRODUCTION: Hypergolic propellants can be released in large amounts during space launch contingencies. Whether propellant-contaminated suit fabric poses a significant risk to rescue crews, due to off-gassing, has not been explored in detail. In this study, we addressed this issue experimentally, exposing space suit fabric to propellants (dinitrogen tetroxide [N2O4] and monomethyl hydrazine [MMH]).METHODS: The NASA Space Shuttle Program Advanced Crew Escape System II (ACES II) is similar to the NASA Orion Crew Survival System (OCSS) and was utilized here. Suit fabric was placed and sealed int

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Xiao, Hong, Yang-Yang Shi, Zhe-Zhu Xu, Lae-Sung Kim, Dong-yang Li, and Sung-Ki Lyu. "Atomization characteristics of gelled hypergolic propellant simulants." International Journal of Precision Engineering and Manufacturing 16, no. 4 (2015): 743–47. http://dx.doi.org/10.1007/s12541-015-0098-x.

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MATSUNO, Shinsuke, Hiroyasu SAITOH, Fumiteru AKAMATSU, and Masashi KATSUKI. "Atomization Characteristics of Liquid Propellant with Hypergolic Ignition." Journal of High Temperature Society 31, no. 1 (2005): 63–68. http://dx.doi.org/10.7791/jhts.31.63.

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Kim, Kyu-Seop, Yehyun Kim, Sangwoo Jung, Junyeong Jeong, and Sejin Kwon. "Research Studies of Impingement Characteristics for Hypergolic Propellant." Journal of the Korean Society of Propulsion Engineers 23, no. 5 (2019): 90–100. http://dx.doi.org/10.6108/kspe.2019.23.5.090.

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Reddy, Gunda, Jian Song, Michael S. Mecchi, and Mark S. Johnson. "Genotoxicity assessment of two hypergolic energetic propellant compounds." Mutation Research/Genetic Toxicology and Environmental Mutagenesis 700, no. 1-2 (2010): 26–31. http://dx.doi.org/10.1016/j.mrgentox.2010.04.019.

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Dissertations / Theses on the topic "Hypergolic propellant"

1

Notaro, Vincent. "Mixing Analysis of Like Doublet Injectors in High Pressure Environments for Gelled Propellant Simulants." University of Cincinnati / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406821648.

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Subervie, Daniel. "NHC-Boranes : amorceurs de photopolymérisation en émulsion et nouveaux matériaux énergétiques." Thesis, Lyon, 2018. http://www.theses.fr/2018LYSE1209/document.

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Synthèse et étude de nouveaux NHC-Boranes pour leurs propriétés énergétiques et leurs rôles en tant que photo co-amorceurs pour la photopolymérisation en émulsion.Depuis la première synthèse de complexes N-Hétérocycliques Boranes (NHC-Borane) stables en 1993, une étude plus générale de propriétés et réactivité n’a débuté que dans le milieu des années 2000. Les domaines d’applications de ces composés qui sont des paires de Lewis vont de la synthèse organique (agent réducteur, hydroboration de liaisons multiples) en passant par la chimie radicalaire (remplacement de l’hydrure de tributylétain, h

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(11150961), Michael J. Baier. "DEVELOPMENT AND CHARACTERIZATION OF HIGH PERFORMANCE AMMONIA BORANE BASED ROCKET PROPELLANTS." Thesis, 2021.

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Historically, hypergolic propellants have utilized fuels based on hydrazine and its<br>derivatives due to their good performance and short ignition delays with the commonly used<br>hypergolic oxidizers. However, these fuels are highly toxic and require special handling<br><div>precautions for their use.</div><div><br></div><div>In recent years, amine-boranes have begun receiving attention as potential alternatives to<br>these more conventional fuels. The simplest of these materials, ammonia borane (AB, NH3BH3)<br>has been shown to be highly hypergolic with white fuming nitric acid (WFNA), with

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(8086121), Alicia Benhidjeb-Carayon. "Reactivity and Hypergolicity of Liquid and Solid Fuels with Mixed Oxides of Nitrogen." Thesis, 2019.

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<div>When combined with common fuel binders, solid hypergolic fuels can simplify the overall complexity of hybrid rocket systems, as the fuel grain can be ignited and reignited without an external power source or external fluid. In addition, with the hypergolic additive embedded in the binder, the flame zone can be placed at the surface of the grain itself, thereby providing heat to the fuel, improving fuel regression rate, and combustion stability and sustainability. Coupled with high grades of mixed oxides of nitrogen (MON), such hypergolically ignited hybrid configurations are considered a

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Books on the topic "Hypergolic propellant"

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Corporation, MSA Research, and United States. Dept. of the Air Force. Space Division. Plans and Projects Directorate, eds. Foam development for hypergolic propellant spill control: Summary engineering report. The Directorate, 1985.

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2

Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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3

Bryan, Palaszewski, O'Leary Robert, and Lewis Research Center, eds. Preliminary assessment of using gelled and hybrid propellant propulsion for VTOL/SSTO launch systems. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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4

G, Barile R., and United States. National Aeronautics and Space Administration., eds. Sample diluter for detecting hypergolic propellants and other toxic or hazardous gases. National Aeronautics and Space Administration, 1997.

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Conference papers on the topic "Hypergolic propellant"

1

Reich, Alton. "System for the Automated Mitigation of Hypergolic Propellant Leaks." In ASME 2012 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/pvp2012-78495.

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Hypergolic liquid rocket propellants consist of fuel and oxidizer liquids stored in separate tanks that ignite when mixed. They are favored for propulsion systems where precise pulsing or throttling is required. High reliability is also insured because the liquid chemicals are stable for long periods of time, and no ignition system is required — the fuel and oxidizer simply need to be brought together. These propellants have relatively high vapor pressures, are toxic, and may be carcinogenic. A pool of the liquid will pose a health, fire, or explosion hazard. Therefore, missiles containing the

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2

KRISHNAN, A., A. PRZEKWAS, and K. GROSS. "Computational analysis of liquid hypergolic propellant rocket engines." In Space Programs and Technologies Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1552.

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3

Davis, C., and C. Davis. "Streamlining spacecraft hypergolic propellant logistics operations at KSC/CCAS." In 33rd Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-2814.

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4

Matsuura, Yoshiki, and Yosuke Tashiro. "Hypergolic Propellant Ignition Phenomenon with Oxidizer Two-Phase Flow Injection." In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-4154.

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Zarbo, Nick, Hatem Belal, and Timothee L. Pourpoint. "Effect of Water and Humidity on Hypergolic Propellant Ignition Delay." In 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3867.

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HABIBALLAH, M., I. DUBOIS, P. GICQUEL, and R. FOUCAUD. "Experimental study of combustion processes involved in hypergolic propellant coaxial injector operation." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3388.

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7

Nufer, Brian. "A Summary of NASA and USAF Hypergolic Propellant Related Spills and Fires." In SpaceOps 2010 Conference: Delivering on the Dream (Hosted by NASA Marshall Space Flight Center and Organized by AIAA). American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-1994.

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8

Nusca, Michael J., and Michael J. McQuaid. "Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines." In 2006 HPCMP Users Group Conference. IEEE, 2006. http://dx.doi.org/10.1109/hpcmp-ugc.2006.14.

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Nusca, M., C. C. Chen, and M. McQuaid. "Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines." In 2007 DoD High Performance Computing Modernization Program Users Group Conference. IEEE, 2007. http://dx.doi.org/10.1109/hpcmp-ugc.2007.17.

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10

Chen, Chiung-Chu, Michael J. Nusca, Anthony J. Kotlar, and Michael J. McQuaid. "Combustion Chamber Fluid Dynamics and Hypergolic Gel Propellant Chemistry Simulations for Selectable Thrust Rocket Engines." In 2009 DoD High Performance Computing Modernization Program Users Group Conference (HPCMP-UGC). IEEE, 2009. http://dx.doi.org/10.1109/hpcmp-ugc.2009.25.

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Reports on the topic "Hypergolic propellant"

1

Thynell, S. T., J. H. Adair, III Goddard, et al. Spray and Combustion of Gelled Hypergolic Propellants for Future Rocket and Missile Engines. Defense Technical Information Center, 2014. http://dx.doi.org/10.21236/ada614447.

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