EXPERIMENTAL VALIDATION OF THE X-RAY DETERMINED PORE SIZE DISTRIBUTION OF POROUS HYBRID MOTOR GRAINS (English)
- New search for: Buckley, J. R.
- New search for: White, R. T.
- New search for: Nelson, G. J.
- New search for: Buckley, J. R.
- New search for: White, R. T.
- New search for: Nelson, G. J.
In:
Hybrid rockets
; 365-374
;
2019
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ISBN:
- Conference paper / Print
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Title:EXPERIMENTAL VALIDATION OF THE X-RAY DETERMINED PORE SIZE DISTRIBUTION OF POROUS HYBRID MOTOR GRAINS
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Contributors:
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Conference:AIAA Propulsion and Energy Forum ; 2019 ; Indianapolis, Ind.
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Published in:Hybrid rockets ; 365-374
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Publisher:
- New search for: Curran Associates, Inc.
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Place of publication:Red Hook, NY
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Publication date:2019
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
- New search for: 55.60
- Further information on Basic classification
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Keywords:
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Classification:
BKL: 55.60 Raumfahrttechnik -
Source:
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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THRUST AUGMENTATION OF AN ADDITIVELY MANUFACTURED HYBRID ROCKET SYSTEM USING SECONDARY H2O2 INJECTIONWhitmore, S. A. / Heiner, M. C. et al. | 2019
- 33
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DIODE LASER IGNITION MECHANISM FOR HYBRID PROPULSION SYSTEMSDyrda, D. M. / Korneyeva, V. / Cantwell, B. J. et al. | 2019
- 49
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NOVEL HYBRID ROCKET INTERNAL BALLISTIC CONFIGURATION WITH COAXIALLY LOCATED TUBE INJECTORKahraman, M. / Gegeoglu, K. / Ozkol, I. / Karabeyoglu, M. A. et al. | 2019
- 66
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POROSITY AND TEMPERATURE EFFECTS ON AXIAL-INJECTION, END-BURNING HYBRIDHitt, M. A. et al. | 2019
- 72
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VIABILITY STUDY OF ACRYLONITRILE BUTADIENE STYRENE POLYMER AS FUEL FOR HYBRID ROCKET ENGINES IN COLOMBIALozada, H. M. / Urrego, J. A. / Fabio, R. M. et al. | 2019
- 89
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DEVELOPMENT OF HAPITH SMALL LAUNCH VEHICLE BASED ON HYBRID ROCKETChen, Y. S. et al. | 2019
- 97
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FEASIBILITY STUDY FOR HYPERSONIC FLIGHT TEST USING A REUSABLE HYBRID ROCKET MOTORNardozzo, P. / Popkin, S. / Smith, J. et al. | 2019
- 109
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DEVELOPMENT OF THE NUCLEUS HYBRID PROPULSION SYSTEM: ENABLING A SUCCESSFUL FLIGHT DEMONSTRATIONFaenza, M. G. / Boiron, A. J. / Haemmerli, B. / Verberne, O. et al. | 2019
- 131
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A SINGLE STAGE TO ORBIT DESIGN FOR A HYBRID MARS ASCENT VEHICLEStory, G. / Schnell, A. / Yaghoubi, D. / Karp, A. / Nakazono, B. / Zilliac, G. et al. | 2019
- 150
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EVALUATION OF SAFETY DISTANCE FOR BLAST OF HYBRID ROCKET PROPELLANTSTakahashi, A. / Kitagawa, K. / Shimada, T. et al. | 2019
- 176
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RESPONSE MECHANISMS IN AXIAL-INJECTION END-BURNING HYBRID ROCKETSSaito, Y. / Tsuji, A. / Yamada, A. / Nagata, H. et al. | 2019
- 186
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SIMULATION OF SURFACE INSTABILITIES IN LIQUEFYING HYBRID ROCKET FUELSKnol, I. M. / Maicke, B. A. et al. | 2019
- 199
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SUPPRESSING THE LFI WITH DUAL FUEL IN HYBRID ROCKET COMBUSTIONChae, H. / Kang, S. H. / Lee, C. et al. | 2019
- 209
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SELECTION CRITERIA FOR TACKIFIER ADDITION TO PARAFFIN WAX BASED HYBRID ROCKET FUELSBilge, K. / Emerce, N. B. / Yildiz, U. C. / Kokal, U. / Baysal, M. et al. | 2019
- 222
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PERFORMANCE ENHANCING ADDITIVES FOR HYBRID ROCKETSKarakas, H. / Kara, O. / Ozkol, I. / Karabeyoglu, A. et al. | 2019
- 236
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EXPERIMENTAL TEST OF N2O/CO2 OXIDIZER MIXTURE WITH PARAFFIN BASED ALUMINUM FUEL FOR MARS ASCENT VEHICLESKara, O. / Karakas, H. / Karabeyoglu, M. A. et al. | 2019
- 253
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LOW PRESSURE IGNITION TESTING OF A HYBRID SMALLSAT MOTORJens, E. T. / Karp, A. C. / Williams, K. / Nakazono, B. / Rabinovitch, J. / Dyrda, D. / Mechentel, F. et al. | 2019
- 264
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STATE OF ART AND CURRENT CHALLENGES OF THE PARAFFIN-BASED HYBRID ROCKET TECHNOLOGYLeccese, G. / Cavallini, E. / Pizzarelli, M. et al. | 2019
- 283
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DEVELOPMENT AND TEST FLIGHT OF THE ATLANTIS I NITROUS OXIDE/PARAFFIN-BASED HYBRID ROCKETMessinger, T. / Hill, C. / Quinn, D. / Stannard, D. / Doerksen, G. / Johansen, C. et al. | 2019
- 293
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AN INVESTIGATION OF THE CENTRIFUGAL CASTING OF PARAFFIN WAX ON EARTH AND IN MICROGRAVITYStober, K. J. / Wanyiri, J. / Sanchez, A. / Hooper, M. / Mazumder, M. / Jiwani, S. / Waft, C. / Lifson, M. / Joseph, C. / Wood, D. et al. | 2019
- 316
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DEMONSTRATION OF AN ALTERNATING-INTENSITY SWIRLING OXISIZER FLOW TYPE 214 HYBRID ROCKET FUNCTIONSNakagawa, I. / Kishizato, D. / Koinuma, Y. / Tanaka, S. et al. | 2019
- 326
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EXPERIMENTAL INVESTIGATION OF ABS-PARAFFIN 3D PRINTED HYBRID ROCKETBresler, J. A. / Natan, B. et al. | 2019
- 342
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DIODE LASER IGNITION TESTING FOR PMMA/GOX HYBRID MOTORSDyrda, D. M. / Mechentel, F. S. / Cantwell, B. J. / Karp, A. C. / Rabinovitch, J. / Jens, E. T. et al. | 2019
- 356
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ROBUST DESIGN OF HYBRID ROCKET ENGINE FOR SMALL SATELLITE LAUNCHERSCasalino, L. / Pastrone, D. / Masseni, F. et al. | 2019
- 365
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EXPERIMENTAL VALIDATION OF THE X-RAY DETERMINED PORE SIZE DISTRIBUTION OF POROUS HYBRID MOTOR GRAINSBuckley, J. R. / White, R. T. / Nelson, G. J. et al. | 2019
- 375
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SPECTROSCOPIC TECHNIQUES FOR MEASURING REGRESSION RATES OF LIQUEFYINGMcDougall, C. C. / Hill, C. D. / Heinrichs, C. J. / Johansen, C. T. et al. | 2019
- 384
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RECONSTRUCTION OF ATTENUATED HYBRID MOTOR CHAMBER PRESSURE SIGNALS USING MAXIMUM LIKELIHOOD ESTIMATION AND OPTIMAL DECONVOLUTIONWhitmore, S. A. / Zelesnik, E. M. et al. | 2019
- 407
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BOUNDARY-LAYER COMBUSTION OF WAX-BASED FUELS AT VARIOUS CHAMBER PRESSURES UNDER TWO STATIC ACCELERATION ENVIRONMENTSOzawa, K. / Yoshino, T. / Wang, H. W. / Tsuboi, N. et al. | 2019
- 430
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AN EXPERIMENTAL STUDY OF FACTORS AFFECTING HYPERGOLIC IGNITION OFClements, K. A. / Baier, M. J. / Ramachandran, P. V. / Son, S. F. et al. | 2019
- 440
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FUEL REGRESSION CHARACTERISTICS IN HYBRID ROCKETS USING N2O/HDPEIto, S. / Kamps, L. / Sakurai, K. / Kageyama, L. / Okuda, T. / Nagata, H. et al. | 2019
- 451
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MEDICAL GRADE N20/02 MIXTURES AS INEXPENSIVE AND VOLUMETRICALLY EFFICIENT OXIDIZERS FOR SMALL SPACECRAFT HYBRID PROPULSION SYSTEMSWhitmore, S. A. / Stoddard, R. L. / Babb, R. S. / Horlacher, D. J. et al. | 2019
- 484
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DEVELOPMENT AND PRELIMINARY TESTING OF PARAFFIN HYBRID ROCKET FUEL GRAINS WITH HELICAL PORT STRUCTURESPabarcius, L. L. B. et al. | 2019
- 495
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CHARACTERISTICS OF SOLID FUEL BASED ON WAX WITH ADDED POLYPROPYLENEKinoshita, K. / Matsumoto, Y. / Takahashi, K. et al. | 2019
- 502
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ALUMINUM POWDER EFFECTS WITH AFT-CHAMBER EXTENSION AND BAFFLE PLATE INSTALLATION FOR HYBRID ROCKETKanbayashi, Y. / Takahashi, K. / Takahashi, A. et al. | 2019
- 511
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SWEATING HYBRID ROCKET FUELS; INCLUSION AND TEMPERATURE ACTIVATED RELEASE OF LIQUID FUELS IN SOLID BINDERSMcClain, M. S. / Paik, M. / Farrell, C. / Youngblood, J. P. / Pourpoint, T. L. et al. | 2019
- 522
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MODIFICATION OF PARAFFIN-BASED HYBRID ROCKET FUELS USING STRUCTURALHill, C. D. / McDougall, C. C. / Messinger, T. L. / Johansen, C. T. et al. | 2019
- 532
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OPTICALLY RESOLVED FUEL REGRESSION OF A CLEAR PMMA HYBRID ROCKETMechentel, F. S. / Hord, B. R. / Cantwell, B. J. et al. | 2019
- 549
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DATA CLUSTERING OF HYBRID ROCKET COMBUSTION FLAMEPetrarolo, A. / Kobald, M. / Ruttgers, A. et al. | 2019
- 565
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NUMERICAL INVESTIGATION OF A LOW THRUST PARAFFIN/N20 HYBRID ROCKETSrivastava, S. / Ingenito, A. / Andriani, R. et al. | 2019
- 581
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RECENT ADVANCEMENTS IN EXPERIMENTAL AND NUMERICAL CHARACTERIZATION OF PARAFFIN-BASED FUELS FOR HYBRID ROCKET APPLICATIONMartino, G. D. Di / Gallo, G. / Mungiguerra, S. / Carmicino, C. / Savion, R. / Cardillo, D. / Battista, F. et al. | 2019
- 593
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PREDICTIVE CFD MODEL FOR INTERNAL BALLISTICS OF HYBRID ROCKET ENGINES USING SUPERCRITICAL PARAFFIN-WAX AND OXYQGENMigliorino, M. T. / Bianchi, D. / Nasuti, F. et al. | 2019
- 609
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EVALUATION OF DISCRETIZATION SCHEMES IN BIGLOBAL STABILITY ANALYSIS OF CYLINDRICALLY-SHAPED SOLID AND HYBRID ROCKETSElliott, T. S. / Sam, A. M. / Grider, T. D. / Majdalani, J. et al. | 2019
- 623
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CFD ANALYSIS OF PARAFFIN-BASED HYBRID ROCKETS WITH COUPLED NOZZLEBianchi, D. / Migliorino, M. T. / Nasuti, F. / Onofri, M. et al. | 2019
- 639
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INVESTIGATION OF GRAPHITE NOZZLE EROSION IN HYBRID ROCKETS USING N2O/HDPEKamps, L. / Sakurai, K. / Ozawa, K. / Nagata, H. et al. | 2019
- 657
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BASIC RESEARCH ON IMPROVEMENT OF COMBUSTION EFFICIENCY OF WAX FUEL HYBRID ROCKETYasuda, K. / Nakagawa, I. et al. | 2019
- 667
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REAL-TIME DEEP THROTTLING TESTS OF A HYDROGEN PEROXIDE HYBRID ROCKET MOTORRuffin, A. / Paccagnella, E. / Santi, M. / Barato, F. / Pavarin, D. et al. | 2019
- 687
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FLIGHT TESTING OF TECHNOLOGY DEMONSTRATOR WITH HYDROGEN PEROXIDE HYBRID ROCKETYun, Y. / Seo, J. / Park, K. / Jeong, J. / Kim, J. / Kwon, S. et al. | 2019
- 695
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DEVELOPMENT OF A 2D OPTICALLY ACCESSIBLE HYBRID ROCKET MOTORBoyle, S. M. / Scarborough, D. E. et al. | 2019
- 706
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EFFECT OF AFT CHAMBER VOLUME ON HYBRID ROCKET COMBUSTION EFFICIENCYKageyama, L. / Kamps, L. / Nagata, H. et al. | 2019
- 721
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PERFORMANCE OF SOLID STATE EMULSIONS OF ISOAMYL ALCOHOL IN EVA-STABILIZED LOW-MW POLYETHYLENE, STRUCTURED BY LASER-SINTERED NYLON SCAFFOLDS AS FUELS IN N2O HYBRID ROCKET ENGINEZdybal, D. / Klos, W. / Drozdz, P. / Rydz, Z. / Kobus, K. / Wyciszkiewicz, B. / Zwolak, A. / Wyzlinski, M. / Tatara, T. / Guzik, A. et al. | 2019
- 740
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EXPERIMENTAL FINDINGS ON PRE- AND POST-COMBUSTION CHAMBER EFFECTS IN A LABORATORY-SCALE MOTORMechentel, F. S. / Cantwell, B. J. et al. | 2019
- 760
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THERMOCHEMICAL STRUCTURE OF A HYBRID ROCKET REACTION LAYER BASED ON LASER ABSORPTION TOMOGRAPHYBendana, F. A. / Castillo, J. J. / Hagstrom, C. G. / Spearrin, R. M. et al. | 2019
- 769
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HYPERGOLIC HYBRID ROCKET MOTOR CHARACTERIZATION WITH MON-25 AT ATMOSPHERIC AND REDUCED PRESSURESBenhidjeb-Carayon, A. / McCormick, J. M. / Yilmaz, C. / Gabl, J. R. / Whitehead, B. E. / Pourpoint, T. L. et al. | 2019
- 788
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CFD MODELING OF A HYBRID ROCKET USING A GENERALIZED ONE-DIMENSIONAL MODEL OF THE FLAME TEMPERATUREUddanti, N. S. / Crispin, Y. et al. | 2019
- 801
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NUMERICAL SIMULATION OF COMBUSTION IN A HYBRID ROCKET WITH LIQUEFYINGPrasad, G. M. D. / Menon, S. / Baran, A. et al. | 2019
- 814
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STUDY OF REGRESSION RATES IN A HYBRID ROCKET MOTORDhanasekaran, J. / Ramanan, V. et al. | 2019
- 821
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THE DEVELOPMENT OF A POWDER-FILLED, ABS MATRIX FOR USE AS FUEL IN A HYBRID ROCKET MOTORAarant, T. / Bass, J. / Grizzel, T. / Holladay, S. / McVey, M. / Putthoff, W. / Shaw, A. / Tarle, P. / Nickel, R. / Little, C. et al. | 2019
- 834
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BURNING BEHAVIOR INVESTIGATION OF A VORTEX FLOW PANCAKE HYBRID ROCKET ENGINEParavan, C. / Lisi, F. / Massimo, P. / Bisin, R. / Galfetti, L. et al. | 2019