Contemporary methods to measure regression rate of energetic materials: A review
Tài liệu tham khảo
Sundaram, 2017, Metal-based nanoenergetic materials: synthesis, properties, and applications, Prog Energy Combust Sci, 61, 293, 10.1016/j.pecs.2017.02.002
Barato, 2016, Integrated approach for hybrid rocket technology development, Acta Astronaut, 128, 257, 10.1016/j.actaastro.2016.07.023
Dreizin, 2009, Metal-based reactive nanomaterials, Prog Energy Combust Sci, 35, 141, 10.1016/j.pecs.2008.09.001
Beckstead, 2007, Modeling of combustion and ignition of solid propellant ingredients, Prog Energy Combust Sci, 33, 497, 10.1016/j.pecs.2007.02.003
DeLuca, 2013, Characterization of HTPB-based solid fuel formulations: performance, mechanical properties, and pollution, Acta Astronaut, 92, 150, 10.1016/j.actaastro.2012.05.002
Tian, 2017, Three-dimensional numerical and experimental studies on transient ignition of hybrid rocket motor, Acta Astronaut, 140, 247, 10.1016/j.actaastro.2017.08.022
Yeh, 1996, Ignition and combustion of boron particles, Prog Energy Combust Sci, 22, 511, 10.1016/S0360-1285(96)00012-3
Kumar, 2014, Measurement of regression rate in hybrid rocket using combustion chamber pressure, Acta Astronaut, 103, 226, 10.1016/j.actaastro.2014.06.044
Gany, 2014, Thermodynamic limitation on boron energy realization in ramjet propulsion, Acta Astronaut, 98, 128, 10.1016/j.actaastro.2014.01.023
Dreizin, 2015, Correlating ignition mechanisms of aluminum-based reactive materials with thermoanalytical measurements, Prog Energy Combust Sci, 50, 81, 10.1016/j.pecs.2015.06.001
Zarko, 1994, Critical review of methods for regression rate measurements of condensed phase systems, 600
Fry, 2001, Solid propellant burning rate measurement methods used within the NATO propulsion community
Gupta, 2015, Various methods for the determination of the burning rates of solid propellants: an overview, Cent Eur J Energy Mater, 12, 593
Pei, 2015, Research progress in the burning rate measurement technology of solid propellant, Chin J Explos Propellants, 38, 9
Carmicino, 2018, Novel comprehensive technique for hybrid rocket experimental ballistic data reconstruction, J Propuls Power, 34, 133, 10.2514/1.B36517
Hessler, 2000, Consistent definitions for burning-rate measurement in solid-rocket motors, Combust Explos Shock Waves, 36, 76, 10.1007/BF02701517
Hessler, 2000, Error analysis of burning-rate measurement procedures, Combust Explos Shock Waves, 36, 96, 10.1007/BF02701518
Deluca, 2019, Burning rate issues in solid rocket propulsion, 268
Novozhilov, 2000, Acoustic resonance upon propellant combustion, Combust Explos Shock Waves, 36, 3, 10.1007/BF02701508
Osborn, 1966, Continuous measurement of solid propellant burning rates, Rev Sci Instrum, 37, 86, 10.1063/1.1719960
Frederick, 1996, Measuring the regression of a burning solid propellant, Rev Sci Instrum, 67, 2903, 10.1063/1.1147070
Osborn, 1963, Photographic measurement of burning rates in solid-propellant rocket motors, Rev Sci Instrum, 34, 305, 10.1063/1.1718345
Eisenreich, 1987, An optical system for measuring the burning rate of solid propellant strands, Propellants Explos Pyrotech, 12, 78, 10.1002/prep.19870120304
Dunn, 2018, Spatially and temporally resolved regression rate measurements for the combustion of paraffin wax for hybrid rocket motor applications, Aerosp Sci Technol, 72, 371, 10.1016/j.ast.2017.11.024
Wang, 1998, Laser technique for determining solid propellant transient burning rates during oscillatory combustion, Fuel, 77, 1845, 10.1016/S0016-2361(98)00104-5
Wang, 2001, A laser technology for measurement of solid propellant transient burning rates during rapid depressurization, Fuel, 80, 263, 10.1016/S0016-2361(00)00087-9
Strand, 1974, Microwave Doppler shift technique for determining solid propellant transient regression rates, J Spacecr Rocket, 11, 75, 10.2514/3.62012
Yin, 1971, Continuous measurement of transient burning rates of composite propellant undergoing rapid depressurization
DeLuca, 2011, Time-resolved burning of solid fuels for hybrid rocket propulsion, Prog Propul Phys, 2, 405, 10.1051/eucass/201102405
Tang, 2017, Mechanical modifications of paraffin-based fuels and effects on combustion performance, Propellants Explos Pyrotech, 42, 1268, 10.1002/prep.201700136
Mason, 1964, Multiple reflection ultrasonic delay lines, 485
Traineau, 1986, Ultrasonic measurements of solid propellant burning rates in nozzleless rocket motors, J Propuls Power, 2, 215, 10.2514/3.22872
Dijkstra, 1990, Ultrasonic regression rate measurement in solid fuel ramjets
RJr, 2000, Review of ultrasonic technique for steady state burning rate measurements
Deepak, 2013, Application of ultrasonic technique for measurement of instantaneous burn rate of solid propellants, Def Sci J, 48, 197, 10.14429/dsj.48.3899
Lestrade, 2015, Liquefying fuel regression rate modeling in hybrid propulsion, Aerosp Sci Techol, 42, 80, 10.1016/j.ast.2014.11.015
Hasegawa, 2010, Novel burning rate measurement technique for solid propellant by means of ultrasonics, Combust Explos Shock Waves, 46, 188, 10.1007/s10573-010-0029-1
Murphy, 2002, Evaluation of ultrasound technique for solid-propellant burning rate response measurements, J Propuls Power, 18, 641, 10.2514/2.5978
Song, 2009, Measurement of solid propellant burning rates by analysis of ultrasonic full waveforms, J Mech Sci Technol, 23, 1112, 10.1007/s12206-009-0302-y
Cauty, 2000, Ultrasound measurement method: errors, noise, and sensitivity, Combust Explos Shock Waves, 36, 54, 10.1007/BF02701514
Hsieh, 1986, Modeling and measuring of erosive burning of stick propellants
Salizzoni, 1993, Temperature sensitivity measurements and regression behavior of a family of boron-based very high burning rate propellants, 438
Tian, 2015, Diagnosis of transient end burning law for gas generator with low burning velocity fuel rich propellant, J Propulsion Technol, 36
Jones, 2016, Overview of X-ray techniques for solid rocket propellant regression measurements
Kohno, 1997, X-ray diagnostics for local burning rate measurement of solid propellants, Int J Energy Mater Chem Propulsion, 4, 918
Hasegawa, 2003, Erosive burning of aluminized composite propellants: x-ray absorption measurement, correlation, and application, J Propuls Power, 22, 975, 10.2514/1.7950
Xiao, 2003, Particle velocity on solid-propellant surface using X-ray real-time radiography, AIAA J, 41, 1763, 10.2514/2.7294
Kuper, 2010, High-resolution X-ray computed tomography of low-contrast samples with the use of synchrotron radiation, 451
Pogany, 1997, Contrast and resolution in imaging with a microfocus X-ray source, Rev Sci Instrum, 68, 10.1063/1.1148194
Hertz, 2009, Laboratory X-ray micro imaging: sources, optics, systems and applications, J Phys Conf Ser, 186, 0120271
Koch, 1953, Reflexion de micro-ondes par des phenomenes de detonation, C R Acad des Sci Paris, 236, 661
Cook, 1955, Measurement of detonation velocity by doppler effect at three-centimeter wavelength, J Appl Phys, 26, 426, 10.1063/1.1722012
Dean, 1967, The use of microwaves for the detection of flaws and measurement of erosion rates in materials, J Sci Instrum, 44, 699, 10.1088/0950-7671/44/9/317
Wood, 1983, Measurement of solid propellant burning rates employing microwave techniques
Strand, 1974, Microwave doppler shift technique for determining solid propellant transient regression rates, J Spacecr Rockets, 11, 75, 10.2514/3.62012
Strand, 1978, A variable-frequency driver microwave transientregression rate measurement system, 155
Strand, 1980, Microwave measurement of the solid-propellant pressure-coupled response function, J Spacecr Rocket, 17, 483, 10.2514/3.57768
Aničin, 1986, Flame plasma and the microwave determination of solid propellant regression rates, Combust Flame, 64, 309, 10.1016/0010-2180(86)90148-3
Bozic, 1997, Measurement system for determining solid rocket propellant burning rate using reflection microwave interferometry, J Propuls Power, 13, 457, 10.2514/2.5197
Bozic, 1998, Measurement system for determining solid propellant burning rate using transmission microwave interferometry, J Propuls Power, 14, 421, 10.2514/2.5318
Zarko, 2000, Methodical problems of solid-propellant burning-rate measurements using microwaves, Combust Explos Shock Waves, 36, 62, 10.1007/BF02701515
Zarko, 2002, Microwaves as a tool for energetic materials characterization
Zarko, 2002, Critical assessment of the microwave method for measuring steady-state and transient regression rates of solids, 725
Zhai, 2019, Non-intrusive burning rate measurements of high-explosives by terahertz interferometry, 367
OYa, 1977, On measurement of mass burning rate in transient combustion of condensed substance using oscillations, Combust Explos Shock Waves, 13, 789, 10.1007/BF00740479
Kochakov, 1978, Transducer for measurement the mass losses upon combustion, Combust Explos Shock Waves, 14, 126, 10.1007/BF00789188
Brill, 1992, Connecting the chemical composition of a material to its combustion characteristics, Prog Energy Combust Sci, 18, 91, 10.1016/0360-1285(92)90019-W
Zarko, 1984
Abrukov, 1983, New possibilities of investigating the combustion processes of condensed systems by interferometry, Combust Explos Shock Waves, 19, 594, 10.1007/BF00750431
Abrukov, 1997, Ignition of propellants: shaping and development of burning wave and its characteristics, Int J Energy Mater Chem Propulsion, 4, 783
Khudyakov, 1967, On measurement of mass burning rate of solid propellants [translation], Fizika Goreniya i Vzryva, 3, 462
Mikheev, 1978, Measurement of burning rates in transient combustion processes under influence of external radiation, 63, 173
Olliges, 2008, Invited article: time accurate mass flow measurements of solid-fueled systems, Rev Sci Instrum, 79, 10.1063/1.2982492
D'Souza, 2005, Investigation of time-dependent forces on a nano-Newton-second impulse balance, Rev Sci Instrum, 76
Perov, 2014, New microwave method for measuring unsteady mass gasification rate of condensed systems, Combust Explos Shock Waves, 50, 739, 10.1134/S0010508214060173
Zarko, 2019, Microwave resonator method for measuring transient mass gasification rate of condensed systems, Acta Astronaut, 158, 272, 10.1016/j.actaastro.2019.03.028
Juhasz, 1976, The closed bomb technique for burning rate measurement at high pressure, 129
Yilmaz, 2008, Solid propellant burning rate from strand burner pressure measurement, Propellants Explos Pyrotech, 33, 109, 10.1002/prep.200800216
Arkhipov, 2000, Applicability conditions for inverse methods of reconstructing nonsteady burning rate, Combust Explos Shock Waves, 36, 318, 10.1007/BF02699383
Ivanov, 2002, Estimate of the dynamic characteristics of unsteady combustion of a solid propellant in a semi-closed volume from measurements of variable pressure, Combust Explos Shock Waves, 38, 71, 10.1023/A:1014014202751
Arkhipov, 2010, Comparative analysis of methods for measuring the transient burning rate. I. Research methods, Combust Explos Shock Waves, 46, 564, 10.1007/s10573-010-0074-9
Mihlfeith, 1972, Propellant combustion instability as measured by combustion recoil, AIAA J, 10, 1280, 10.2514/3.50372
Simonenko, 1981, Reactive force of combustion products as a measure of the transient burning rate of a propellant, Fizika Goreniya i Vzryva, 17, 129
Zanotti, 1993, Experimental and numerical approach to the study of the frequency response of solid propellants, Combust Explos Shock Waves, 29, 286, 10.1007/BF00797642
Finlinson, 1994, Laser recoil, plume emission, and flame height combustion response of HMX and RDX at atmospheric pressure, 1645
Brewster, 1997, Laser-recoil combustion response of RDX, Combust Sci Techol, 122, 362, 10.1080/00102209708935616
Zhang, 2005, Development of a low-temperature co-fired ceramic solid propellant microthruster, J Micromech Microeng, 15, 944, 10.1088/0960-1317/15/5/007
Orieux, 2002, Thrust stand for ground tests of solid propellant microthrusters, Rev Sci Instrum, 73, 2694, 10.1063/1.1483901
Kiskin, 2000, Special features of implementation of the recoil-force registration method for burning-rate measurement, Combust Explos Shock Waves, 36, 48, 10.1007/BF02701513
Kiskin, 2016, Sensor of small forces with extended frequency range and compensation of perturbations of environment, Combust Plasma Chem, 14, 279
Kiskin, 2000, Verifying the recoil force vs. burning rate dependence, Combust Explos Shock Waves, 36, 39, 10.1007/BF02701512
Hermance, 1967, Continuous measurement of the burning rate of a composite solid propellant, AIAA J, 5, 1775, 10.2514/3.4303
Yin C.F., Hermance C.E. Continuous measurement of transient burning rates of a composite propellant undergoing rapid depresurization. AIAA Paper 1971-173, 10.2514/6.1971-173.
Monti, 1978, Continious regression rate measurement in hybrid rockets, 63, 111
De Zilwa, 2004, Time-resolved fuel-grain port diameter measurement in hybrid rockets, J Propuls Power, 20, 10.2514/1.2188
Hashmi M.A., Chandran Subash B.S., Chakravarthy S.R., Rathi R., Ganesan S., Jayaraman K. Sensitivity analysis of solid propellant burn rate measurements using ultrasound technique by different data deduction methods. AIAA Paper 2019 4295. DOI 10.2514/6.2019-4295.
Kalman, 2018, Synchrotron-based measurement of aluminum agglomerates at motor conditions, Combust Flame, 196, 144, 10.1016/j.combustflame.2018.06.013
Kellogg, 2019, Synchrotron based measurement of the temperature dependent thermal expansion coefficient of ammonium perchlorate, Propellants Explos Pyro, 45
Glotov, 2002, Ignition and combustion characteristics of propellants containing coated aluminum particles, P80
Kiskin, 2006, Simulation of the spectrum of recoil force oscillations during combustion of composites propellants, Khimicheskaya Fizika, 25, 66
Arkhipov, 2014, Laboratory method for measurement of the specific impulse of solid propellants, Combust Explos Shock Waves, 50, 622, 10.1134/S0010508214050177
Frederick, 1996, Laboratory-scale hybrid rocket motor uncertainty analysis, J Propuls Power, 12, 605, 10.2514/3.24076
Mezroua A., Lefebvre M.H., Trache D., Khimeche K. Burning Rate of PVC Plastisol Composite Propellants and Correlation Between Closed Vessel and Strand Burner Tests Data. In: Pang W, DeLuca L, Gromov A, Cumming A. (Eds) Innovative Energetic Materials: Properties, Combustion Performance and Application. Springer, Singapore. 2020; 351-372. https://doi.org/10.1007/978-981-15-4831-4_12.
Rajak R., Chakravarthy S.R., Ganesan S. Measurement of admittance and acoustic augmentation of burning rate of composite solid propellants using Laser Doppler Velocimetry. Proc Comb Institute 2021;38(3):4391-4399.