46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 2010
Nashville, Tennessee, USA
25 – 28 July 2010
Volume 1 of 7
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VOLUME 1
EJECTOR/ENGINE/NACELLE INTEGRATION FOR INCREASED THRUST MINUS DRAG ...... 1 S. Khalid, J. Sokhey
POWERED MODEL WIND TUNNEL TESTS OF A HIGH-OFFSET SUBSONIC TURBOPROP AIR INTAKE ...... 12 L. Ruiz-Calavera, D. Funes-Sebastian, D. Perdones-Diaz
PROPULSION TECHNOLOGY LIFECYCLE OPERATIONAL ANALYSIS ...... 29 J. Robinson, R. Rhodes
PROPULSION SYSTEM CHOICES AND THEIR IMPLICATIONS ...... 48 C. Joyner II, D. Levack, R. Rhodes, J. Robinson
CRITICAL TEMPERATURE DETERMINATIONS FOR THE LEAD-FREE PRIMARY EXPLOSIVES DBX-1 AND KDNP ...... 76 W. Sanborn, J. Fronabarger, M. Williams
RELATIONSHIP BETWEEN ARRHENIUS FREQUENCY FACTOR (A) CHARACTERISTICS AND THE DEFLAGRATION-TO-DETONATION TRANSITION (DDT) ...... 90 L. Yang
ORBITAL ANALYSIS OF MACRON PROPULSION...... 115 J. Schonig, A. Ketsdever, D. Kirtley
DEVELOPMENT OF A MICROWAVE CUSP ACCELERATOR DRIVEN BY ELECTRON CYCLOTRON RESONANCE ...... 128 B. Sommers, J. Foster
IMPROVED PERFORMANCE OF THE ECR WAVEGUIDE PLASMA CATHODE WITH PERMANENT MAGNETS...... 136 B. Weatherford, J. Foster
EVALUATION AND OPTIMIZATION OF AN 8-GHZ MICROWAVE ELECTROTHERMAL THRUSTER ...... 150 D. Clemens, M. Micci, S. Bilen, J. Hopkins, J. Blum, C. Deforce, S. Chianese
MULTIPLEXED ELECTROSPRAY FOR SPACE PROPULSION APPLICATIONS ...... 161 G. Lenguito, J. Mora, A. Gomez
A 2-STAGE CYLINDRICAL HALL THRUSTER FOR AIR BREATHING ELECTRIC PROPULSION ...... 172 K. Diamant
NEW APPROACH TO NUMERICAL ANALYSIS OF THE HALL THRUSTER ...... 181 K. Kwon, D. Mavris, M. Walker
A PRELIMINARY STUDY OF KRYPTON LASER-INDUCED FLUORESCENCE...... 200 W. Hargus Jr.
ADVANCED HYBRID MODELING OF HALL THRUSTER PLUMES ...... 211 T. Huismann, I. Boyd
LIF VELOCITY MEASUREMENT OF SPUTTERED BORON ATOMS FROM BORON NITRIDE TARGET...... 226 L. Tao, A. Yalin
DESIGN OF A MICROWAVE ASSISTED DISCHARGE INDUCTIVE PLASMA ACCELERATOR...... 233 A. Hallock, K. Polzin
VISCOUS LOSSES IN PLASMA ACCELERATORS...... 242 P. Madhavi, A. Sheshadri
INVESTIGATION OF A GALLIUM MPD THRUSTER WITH AN ABLATING CATHODE ...... 252 R. Thomas, R. Burton, K. Polzin
EVALUATION OF DISCHARGE BEHAVIOR OF THE PULSED PLASMA THRUSTER SIMP-LEX...... 268 T. Schonherr, K. Komurasaki, R. Kawashima, Y. Arakawa, G. Herdrich
ADVANCED SCALING MODEL FOR SIMPLIFIED THRUST AND POWER SCALING OF AN APPLIED- FIELD MAGNETOPLASMADYNAMIC THRUSTER ...... 280 G. Herdrich, A. Boxberger, D. Petkow, R. Gabrielli, S. Fasoulas, M. Andrenucci, R. Albertoni, F. Paganucci, P. Rossetti
NUMERICAL INVESTIGATION OF UNSTEADY FLOW PHENOMENA IN AN HP AXIAL FLOW COMPRESSOR INCORPORATING STATOR SHROUD CAVITIES' ...... 299 T. Frobel, H. Kau, C. Groth, V. Gummer
A DIRECT NUMERICAL SIMULATION OF STATOR-ROTOR INTERACTION IN AN AXIAL COMPRESSOR...... 312 M. Rai
A COMPUTATIONAL INVESTIGATION OF VANE CLOCKING EFFECTS ON EMBEDDED COMPRESSOR STAGE EFFICIENCY...... 334 J. Salontay, N. Key, R. Fulayter
FORCED RESPONSE ANALYSIS OF AERODYNAMICALLY ASYMMETRIC CASCADES...... 344 K. Ekici, R. Kielb, K. Hall
PARAMETRIC STUDY OF UNSTEADY TURBINE PERFORMANCE DRIVEN BY A PULSE DETONATION COMBUSTOR...... 360 K. Rouser, P. King, F. Schauer, R. Sondergaard, J. Hoke
FUEL CELL HYBRID PROPULSION CHALLENGES AND OPPORTUNITIES FOR COMMERCIAL AVIATION...... 372 B. Roth, R. Giffin III
HYBRID EVOLUTIONARY METHOD FOR OPTIMIZATION OF MIXED-FLOW CIVIL TURBOFAN ...... 387 L. Casalino, D. Pastrone
MAIN EFFECTS OF INTERCOOLING AND REGENERATION ON AERONAUTICAL GAS TURBINE ENGINES ...... 397 R. Andriani, F. Gamma, U. Ghezzi
A HISTORICAL SYSTEMS STUDY OF LIQUID ROCKET ENGINE THROTTLING CAPABILITIES...... 405 E. Betts, R. Federick Jr.
A HISTORICAL STUDY OF PAYLOAD MASSES TO EARTH ORBIT AND BEYOND...... 423 R. McNutt Jr.
SACADURA CABRAL AND THE DAWN OF PORTUGUESE AVIATION ...... 430 F. Neves, J. Barata, A. Silva
GASEOUS OXYGEN INJECTION EFFECTS IN HYBRID LABSCALE ROCKET MOTOR OPERATIONS ...... 442 S. Gomes, L. Rocco Jr., J. Rocco, K. Iha
VISUALIZATION OF FLAMES IN COMBUSTION CHAMBER OF SWIRLING-OXIDIZER-FLOW-TYPE HYBRID ROCKET ENGINES...... 452 M. Masugi, T. Ide, S. Yuasa, T. Sakurai, N. Shiraishi, T. Shimada
MEASUREMENT OF AXIAL-DIRECTION FUEL REGRESSION RATE OF SWIRLING-OXIDIZER-FLOW- TYPE HYBRID ROCKET ENGINES...... 460 C. Sezaki, M. Sakamoto, K. Hirata, S. Yuasa, T. Sakurai, N. Shiraishi
EXHAUST GAS ANALYSIS OF A VORTEX OXIDIZER INJECTION HYBRID ROCKET MOTOR ...... 467 D. Myre, P. Caton, J. Cowart, C. Jones
ANALYSIS OF A LOW-EMISSION COMBUSTION STRATEGY FOR A HIGH PERFORMANCE TRANS- ATMOSPHERIC AIRCRAFT ENGINE...... 482 S. Amabile, L. Cutrone, F. Battista, R. Tuccillo
ACOUSTICALLY DRIVEN COMBUSTION INSTABILITIES IN DUMP COMBUSTORS ...... 499 A. Ghosh, S. Park, K. Yu
PERMEATION OF INERT AND SUPERCRITICAL REACTIVE FLUIDS THROUGH METALLIC AND COMPOSITE MEDIA...... 512 N. Gascoin, G. Fau, J. Bioud, P. Gillard
ANALYTICAL METHODOLOGIES FOR HYPERSONIC PROPULSION ...... 529 B. Maicke, J. Majdalani
EXPERIMENTAL INVESTIGATION OF THE SHORT ISOLATOR WITH THE RAMP UNDER ASYMMETRIC INCOMING FLOW...... 546 X. Cao, K. Zhang
CFD MODELING OF AN ISOLATOR SHOCK TRAIN IN A SCRAMJET ENGINE ...... 554 T. Hoeger, P. King, D. Decker, J. Donbar, S. Cox-Stouffer
HIGH-FREQUENCY PRESSURE MEASUREMENTS FOR UNSTART DETECTION IN SCRAMJET ISOLATORS...... 565 J. Donbar, G. Linn, S. Srikant, M. Akella
UTILIZATION OF UNIVERSAL CONTROLS ANALYSIS TOOL AND CFD IN PARALLEL FOR A COLD NOZZLE FLOW ...... 582 J. Faure, S. Chintalapati, N. Divitotawela, D. Kirk, H. Gutierrez
A HISTORY OF COLLAPSE FACTOR MODELING AND EMPIRICAL DATA FOR CRYOGENIC PROPELLANT TANKS...... 593 L. Quay, B. Hodge
PROGRESS IN MODELING PRESSURIZATION IN PROPELLANT TANKS ...... 622 S. Mattick, C. Lee, A. Hosangadi, V. Ahuja
COMPUTATIONAL MODEL OF THE CHILLDOWN AND PROPELLANT LOADING OF THE SPACE SHUTTLE EXTERNAL TANK ...... 635 A. Leclair, A. Majumdar
A STUDY OF THE APPLICATION OF A FINITE ELEMENT MODEL TO THE PREDICTIONS OF THE INJECTION-COUPLED RESPONSE OF A LOX POST...... 644 R. Lin, F. Bertolotti, C. Eckett, T. Hinerman, R. Jensen
COMPUTATIONAL STUDIES OF THE EFFECTS OF OXIDIZER INJECTOR LENGTH ON COMBUSTION INSTABILITY...... 650 R. Smith, G. Xia, W. Anderson, C. Merkle
LARGE EDDY SIMULATION OF HIGH-FREQUENCY COMBUSTION INSTABILITY OF SUPERCRITICAL LOX/GH2 FLAME...... 672 S. Matsuyama, J. Shinjo, S. Ogawa, Y. Mizobuchi
ATMOSPHERIC MINING IN THE OUTER SOLAR SYSTEM: UNIVERSITY STUDIES OF MINING VEHICLES AND PROPULSION ...... 682 B. Palaszewski
ELECTRON-CYCLOTRON RESONANCE PROPULSION ...... 703 J. Brainerd, A. Reisz
COUPLED GRAVITATIONAL FIELDS: A NEW PARADIGM FOR PROPULSION SCIENCE ...... 714 W. Droscher, J. Hauser
INERTIAL CONFINEMENT FUSION PROPULSION FOR DEEP SPACE MISSIONS REVISITED ...... 728 G. Miley, X. Yang, K. Flippo
L1 TO MARS: A COMBINED ROBOTIC/PILOTED MARS MISSION ...... 741 B. Cassenti
MODELING TWO-PHASE FLOW WITH STOCHASTIC AGGLOMERATION/BREAKAGE MODEL ...... 751 K. Park, G. Xia, S. Heister
LES OF SCALAR MIXING IN A DILUTE SPRAY JET...... 772 S. Srinivasan, S. Menon
COMPUTATIONAL ANALYSIS OF A SLINGER ATOMIZER...... 782 C. Sescu, B. Kuchinschi, A. Sescu, A. Afjeh
ON THE EFFECTS OF IGNITER JETS DURING PRE-IGNITION TRANSIENT OF SRMS ...... 794 B. Favini, S. Zaghi, A. Mascio, E. Cavallini, V. Ferretti, F. Serraglia, M. Giacinto
APPLICATION OF LASER-ASSISTED COMBUSTION TO SOLID PROPELLANT FOR SPACE PROPULSION...... 811 A. Kakami, S. Terashita, T. Tachibana
A STUDY ON AN IGNITION CONTROL TECHNIQUE FOR SYSTEM AUTOMATION OF STATIC TEST ...... 820 S. Lee, J. Ha, Y. Lee
DEVELOPMENT OF ADN-BASED MINIMUM SMOKE PROPELLANTS ...... 826 N. Wingborg, S. Andreasson, J. Flon, M. Johnsson, M. Liledahl, C. Oscarsson, A. Pettersson, M. Wanhatalo
AN IONIC LIQUID-BASED NEXT GENERATION DOUBLE BASE PROPELLANT STABILIZER ...... 834 M. Forton, J. Sims, R. Askins, W. Stevenson, J. Shamshina, M. Smiglak, R. Rogers, R. Barrow
INVESTIGATION IN ENERGETIC MATERIALS COMBUSTION: TOWARDS THE EXPERIMENTAL AND SIMULATED SOLID PROPELLANT FLAME STRUCTURE COMPARISON ...... 842 F. Cauty
DEVELOPMENT OF COMPOSITE SOLID PROPELLANTS BASED ON DICYCLOPENTADIENE BINDER ...... 850 S. Bluestone, S. Heister, S. Son, B. Austin Jr.
AERODYNAMIC PROPULSION INTEGRATION FOR SUPERSONIC BUSINESS JETS ...... 864 T. Berens
AERODYNAMICS IN A HYDROGEN ATMOSPHERE: SUPERSONIC TUBE VEHICLE...... 877 A. Miller
PERFORMANCE COMPARISON OF A FULL-LENGTH AND A TRUNCATED AEROSPIKE NOZZLE...... 886 T. Ladeine, H. Chen
MARS ENTRY, DESCENT, AND LANDING: EXPERIMENTS WITH MULTIPLE ENGINE SUPERSONIC RETRO PROPULSION CONFIGURATION ...... 908 B. Palaszewski, T. Bencic
VOLUME 2
USING THE TWO-BURN ESCAPE MANEUVER FOR FAST TRANSFERS IN THE SOLAR SYSTEM AND BEYOND ...... 925 R. Adams, G. Richardson
ELECTRON CYCLOTRON RESONANCE PROPULSION...... 938 J. Brainerd, A. Reisz
APPLICATION OF POROUS METALS TO SEPARATIONS ...... 949 T. Abensur
PYROTECHNIC VALVE: DESIGN PROCESS AND LESSONS LEARNED...... 958 W. Kurkoski
INVESTIGATING PREMATURE IGNITION OF THRUSTER PRESSURE CARTRIDGES BY VIBRATION- INDUCED ELECTROSTATIC DISCHARGE ...... 970 S. Woods, R. Saulsberry
PROGRESS ON A SIMPLE ANALYTIC MODEL FOR INTERPLANETARY SOLAR ELECTRIC LOW THRUST TRAJECTORIES ...... 985 D. Oh, D. Landau
PRELIMINARY ASSESSMENT OF DETACHMENT IN A PLASMA THRUSTER MAGNETIC NOZZLE...... 1011 E. Ahedo, M. Merino
ELECTRIC PROPULSION FOR SMALL BODY MISSIONS ...... 1023 J. Dankanich
THE INFLUENCE OF INDUCED CURRENTS ON MAGNETIC NOZZLE ACCELERATION AND PLASMA DETACHMENT ...... 1040 J. Little, E. Choueiri
ADVANCES IN MICROCAVITY DISCHARGE THRUSTER TECHNOLOGY ...... 1054 M. Chadenedes, D. Ahern, J. Alaimo, J. Cho, S. Park, J. Eden, R. Burton, J. Yoon, S. Garrett, H. Sitaraman, L. Raja, J. Laystrom- Woodard, G. Benavides, D. Carroll
PERFORMANCE OF THE MINIATURE AND LOW POWER MICROWAVE DISCHARGE ION ENGINE µ1 ...... 1064 H. Koizumi, H. Kuninaka
EFFECT OF ASPECT RATIO ON THE WETTABILITY AND ELECTROSPRAY PROPERTIES OF POROUS TUNGSTEN EMITTERS WITH THE IONIC LIQUID [EMIM][IM] ...... 1071 B. Ticknor, J. Anderson, B. Fritz, Y. Chiu
MACH 2 SIMULATIONS OF A MICRO-LASER ABLATION PLASMA THRUSTER WITH NOZZLES...... 1082 R. Thompson, T. Moeller
DIRECT-DRIVE PERFORMANCE OF A T-100 HET POWERED BY TRIPLE JUNCTION, HIGH-VOLTAGE CONCENTRATOR PV ARRAY...... 1093 H. Brandhorst Jr., S. Best, J. Rodiek, M. O'Neill, M. Piszczor Jr.
EFFECT OF THE MAGNETIC FIELD ON THE PLASMA PLUME OF THE CYLINDRICAL HALL THRUSTER WITH PERMANENT MAGNETS ...... 1099 Y. Raitses, J. Gayoso, E. Merino, N. Fisch
HIGH-SPECIFIC IMPULSE OPERATION OF THE BPT-4000 HALL THRUSTER FOR NASA SCIENCE MISSIONS...... 1104 R. Hofer
CONTROL DESIGN FOR A GENERIC COMMERCIAL AIRCRAFT ENGINE ...... 1119 J. Csank, R. May, J. Litt, T. Guo
A HIGH-FIDELITY SIMULATION OF A GENERIC COMMERCIAL AIRCRAFT ENGINE AND CONTROLLER...... 1133 R. May, J. Csank, T. Lavelle, J. Litt, T. Guo
PERSPECTIVE FOR DISTRIBUTED INTELLIGENT ENGINE CONTROLS OF THE FUTURE ...... 1149 A. Behbahani, B. Tulpule
FLIGHT-TESTING OF PRESSURE REGULATED HYDROGEN-PEROXIDE HYBRID ROCKET TECHNOLOGY DEMONSTRATOR...... 1167 J. Tsohas, A. Rettenmaier, M. Walker, T. Manship, S. Heister
HYBRID PROPULSION SYSTEMS FOR FUTURE SPACE APPLICATIONS...... 1190 F. Martin, A. Chapelle, O. Orlandi, P. Yvart
A TWO-STAGE, SINGLE PORT HYBRID PROPULSION SYSTEM FOR A MARS ASCENT VEHICLE ...... 1211 A. Chandler, B. Cantwell, G. Hubbard, A. Karabeyoglu
TESTING HYPERGOLIC IGNITION OF PARAFFIN WAX/LIALH4 MIXTURES...... 1217 J. Desain, T. Curtiss, K. Metzler, B. Brady
DEVELOPMENT OF LOW COST FUELS FOR HYBRID ROCKET ENGINE ...... 1236 A. Aoki, A. Fukuchi
CHARACTERIZATION OF AMMONIA BORANE (NH3BH3) ENHANCEMENT TO A PARAFFIN FUELED HYBRID ROCKET SYSTEM ...... 1247 M. Weismiller, T. Connell Jr., G. Risha, R. Yetter
HYDRAULIC AND KINEMATIC SYSTEM MODEL FOR TBCC DYNAMIC SIMULATION ...... 1259 E. Gamble, D. Haid
THERMAL MANAGEMENT AND FUEL SYSTEM MODEL FOR TBCC DYNAMIC SIMULATION ...... 1277 E. Gamble, D. Haid
SUPERSONIC FREE-JET COMBUSTION IN A RAMJET BURNER ...... 1291 C. Trefny, V. Dippold III
EFFECT OF A VENT SLOT MIXER WITH A PLASMA JET TORCH IN UNHEATED SUPERSONIC FLOW ...... 1315 C. Kim, I. Jeung, B. Choi, T. Kouchi, G. Masuya
PENETRATION CHARACTERISTICS OF PULSED INJECTION INTO SUPERSONIC CROSSFLOW ...... 1326 T. Kouchi, K. Sasaya, J. Watanabe, H. Sibayama, G. Masuya
EXPERIMENTAL AND NUMERICAL STUDY OF A SUPERSONIC COMBUSTION CHAMBER WITH DIFFERENT TWO-STAGED INJECTION CONCEPTS...... 1336 J. Vellaramkalayil, T. Scheuermann, S. Winkler, J. Wolfersdorf, M. Banica
THE NASA IN-SPACE PROPULSION TECHNOLOGY PROJECT’S CURRENT PRODUCTS AND FUTURE DIRECTIONS...... 1348 D. Anderson, E. Pencil, L. Liou, J. Dankanich, M. Munk, D. Hahne
DEVELOPMENT TESTING OF A NEW BIPROPELLANT PROPULSION SYSTEM FOR THE GMP-T SPACECRAFT ...... 1367 A. Devereaux, F. Cheuret
FINAL OPERATION OF KAGUYA...... 1380 I. Masuda, H. Kagawa, D. Goto, H. Minamino, K. Kajiwara, Y. Kishino, M. Tamura, M. Takahashi, Y. Iwayama, S. Ikegami, M. Miyata
ON THE BIDIRECTIONAL VORTEX WITH ARBITRARY ENDWALL VELOCITY...... 1391 G. Akiki, J. Majdalani
KINETIC SIMULATION OF HYDROGEN COMBUSTION IN A HOMOGENEOUS REACTOR ...... 1403 R. Goncalves, L. Ferrao, R. Rocha, F. Machado, K. Iha, J. Rocco
TRANSIENT THREE-DIMENSIONAL SIDE LOAD ANALYSIS OF OUT-OF-ROUND FILM COOLED NOZZLES ...... 1411 T. Wang, J. Lin, J. Ruf, M. Guidos
VALIDATION OF SUPERSONIC FILM COOLING MODELING FOR LIQUID ROCKET NOZZLE APPLICATIONS...... 1435 C. Morris, J. Ruf
FLOW SEPARATION CHARACTERISTICS OF A THRUST OPTIMIZED PARABOLIC NOZZLE IN A HIGH ALTITUDE SIMULATION CHAMBER...... 1456 S. Verma, O. Haidn
EXPERIMENTAL AND NUMERICAL STUDIES ON TWO-DIMENSIONAL LINEAR PLUG NOZZLE ...... 1469 J. Li, Y. Liu, Y. Liao, C. Wang, Y. Wang, N. Wang
NASA ARES I LAUNCH VEHICLE FIRST STAGE ROLL CONTROL SYSTEM COLD FLOW DEVELOPMENT TEST PROGRAM OVERVIEW ...... 1501 A. Butt, C. Popp, K. Holt, H. Pitts
IMPROVEMENTS IN NANOPARTICLE DISPERSION METHODS FOR SOLID PROPELLANTS...... 1529 D. Reese, S. Son, N. Lacevic, D. Naud
FEASIBILITY STUDY AND PERFORMANCE ASSESSMENT OF A MYRIADE PROPULSION MODULE WITH AN ADN-BASED GREEN MONOPROPELLANT...... 1545 M. Lange, M. Holzwarth, G. Schulte, M. Peukert, O. Feindt
EXPERIMENTAL SWIRL INJECTOR STABILITY CHARACTERIZATION AND COMBUSTION IMAGING...... 1555 R. Ikard, R. Frederick Jr.
EFFECTS OF VARIABLE CHAMBER PRESSURE ON SWIRL COAXIAL INJECTION: A COLD FLOW STUDY...... 1565 C. Eberhart, D. Lineberry, M. Moser
LIQUID OXYGEN / LIQUID METHANE CO-AXIAL SWIRL INJECTOR DEVELOPMENT...... 1577 C. Bostwick, T. Gibbs, E. Besnard
EXCITATION/DETECTION STRATEGIES FOR OH PLANAR LASER-INDUCED FLUORESCENCE MEASUREMENTS IN THE PRESENCE OF INTERFERING FUEL SIGNAL AND ABSORPTION EFFECT ...... 1592 C. Heath, R. Anderson, Y. Hicks, R. Locke
STUDY OF FLAME DYNAMICS AND FLASHBACK MECHANISM IN A GAS TURBINE COMBUSTOR USING SIMULTANEOUS OH-PLIF AND PIV ...... 1610 S. Hosseini, R. Szasz, P. Iudiciani, L. Fuchs, A. Lantz, R. Collin, M. Alden, E. Gutmark
CONCENTRATION AND TEMPERATURE MEASUREMENTS IN TRANSCRITICAL CARBON DIOXIDE JETS...... 1620 P. Seebald, P. Sojka
MEASUREMENT OF LOCAL DENSITY FLUCTUATIONS FOR COMBUSTION DIAGNOSTICS OF DIFFERENT FLAMES USING DUAL LASER VIBROMETRY ...... 1630 S. Koberl, M. Heimel, F. Giuliani, J. Woisetschlager, F. Fontaneto
STUDY ON VALVE SYSTEMS FOR PULSE DETONATION ENGINES ...... 1640 K. Matsuoka, M. Esumi, J. Kasahara, S. Ogawa
DESIGN AND SYSTEM IMPLEMENTATION CONSIDERATIONS FOR HIGH-TEMPERATURE DISTRIBUTED ENGINE CONTROL ...... 1650 J. Tooley, K. Le, S. Parameswaran, A. Behbahani
STABILITY ANALYSIS OF ARINC 825-BASED PARTIALLY DISTRIBUTED AIRCRAFT ENGINE CONTROL WITH TRANSMISSION DELAYS AND PACKET DROPOUTS...... 1673 R. Belapurkar, R. Yedavalli, P. Paluszewski, W. Greene
BURNING AND IGNITION CHARACTERISTICS OF SINGLE ALUMINUM AND MAGNESIUM PARTICLE...... 1682 J. Lim, H. Yang, W. Yoon, D. Lee
FUNDAMENTAL SIMULATION OF ALUMINUM DROPLET COMBUSTION ...... 1690 E. Washburn, M. Gross, S. Smith, S. Balachandar
REACTION OF ALUMINUM IN GAS PHASE NEAR BURNING SURFACE OF AP COMPOSITE PROPELLANTS...... 1705 T. Kuwahara, T. Mano, K. Takahashi, M. Tanabe
HOT GAS FLOW AROUND BURNING ALUMINUM PARTICLES NEAR BURNING SURFACE OF AP COMPOSITE PROPELLANT ...... 1712 K. Takahashi, T. Mano, M. Tanabe, T. Kuwahara, T. Shimada
A NEW CONCEPT AND DESIGN ASPECTS OF AN 'ANTIGRAVITY' PROPULSION MECHANISM BASED ON INERTIAL FORCES...... 1720 C. Provatidis, V. Tsiriggakis
A POSSIBLE EINSTEIN-HEISENBERG EXPLANATION OF ELECTROMAGNETICALLY INDUCED REACTIONLESS PROPULSION EFFECTS ...... 1728 H. Brito
THRUST EVALUATION OF MAGNETO PLASMA SAIL BY USING THREE-DIMENSIONAL HYBRID PIC CODE...... 1743 Y. Kajimura, I. Funaki, I. Shinohara, H. Usui, H. Yamakawa
COMPARISONS IN PERFORMANCE OF ELECTROMAGNET AND PERMANENT-MAGNET CYLINDRICAL HALL-EFFECT THRUSTERS ...... 1752 K. Polzin, Y. Raitses, J. Gayoso, N. Fisch
ELECTRIC PROPULSION THRUSTER ASSEMBLY FOR SMALL GEO ...... 1759 O. Duchemin, V. Leroi, V. Vial, M. Oberg, E. Bourguignon, T. Scalais, A. Demaire, H. Lubberstedt
HALL THRUSTER CHANNEL WALL EROSION RATE MEASUREMENT METHOD USING MULTILAYER COATING CHIP...... 1767 S. Cho, S. Yokota, K. Hara, D. Takahashi, A. Kobayashi
DEMONSTRATION OF 10,400 HOURS OF OPERATION ON 4.5 KW QUALIFICATION MODEL HALL THRUSTER ...... 1777 K. Grys, A. Mathers, B. Welander, V. Khayms
MODELING NEUTRAL DENSITIES DOWNSTREAM OF A GRIDDED ION THRUSTER ...... 1787 G. Soulas
THRUST STAND CHARACTERIZATION OF THE NASA NEXT THRUSTER...... 1819 K. Diamant, J. Pollard, M. Crofton, M. Patterson, G. Soulas
BARIUM DEPLETION IN THE NSTAR DISCHARGE CATHODE AFTER 30,472 HOURS OF OPERATION...... 1837 J. Polk, A. Capece, I. Mikellides, I. Katz
ENTROPY CONSIDERATIONS ON INTEGRATION OF PRESSURE GAIN COMBUSTORS...... 1853 M. Yu, S. Heister
VOLUME 3
FLAME-VORTEX BREAKDOWN INTERACTION IN STABLE AND UNSTABLE COMBUSTION...... 1872 R. Villalva, Y. Perelstein, E. Gutmark
REDUCED CHEMICAL KINETIC MECHANISM FOR JET FUEL COMBUSTION ...... 1886 H. Wang, J. Jin
HARMONIC BALANCE ANALYSIS OF LIMIT CYCLE OSCILLATIONS IN TURBOMACHINERY ...... 1896 K. Ekici, K. Hall
EFFECTS OF INLET DISTORTION ON AEROMECHANICAL STABILITY OF A FORWARD-SWEPT HIGH-SPEED FAN...... 1915 G. Herrick
MIXTURES OF NITROUS OXIDE, CARBON DIOXIDE AND OXYGEN AS OXIDIZERS FOR MARS APPLICATIONS...... 1925 A. Karabeyoglu
LIMIT CYCLE INVESTIGATIONS OF PULSE DETONATION COMBUSTOR FOR PULSE DETONATION TURBINE ENGINE ...... 1936 F. Ma, T. Lavertu, V. Tangirala
ESTIMATION OF PDE PERFORMANCE USING A PULSED LIMIT CYCLE UNSTEADY COMBUSTION CALCULATION ...... 1946 T. Lavertu, F. Ma, V. Tangirala
A SIMPLIFIED MODEL FOR DETONATION BASED PRESSURE-GAIN COMBUSTORS...... 1959 D. Paxson
EXPERIMENTAL STUDIES ON FLAME STABILITY OF A FUELED CAVITY IN A SUPERSONIC CROSSFLOW...... 1970 G. Retaureau, S. Menon
STUDIES ON DYNAMIC CHARACTERISTICS OF REACTING FLOW-FIELDS IN THE LIQUID-FUELED MODEL COMBUSTOR WITH A V-GUTTER TYPE FLAME HOLDER...... 1986 B. Park, S. Kim, W. Yoon, Y. Hwang, H. Yoon
EXPERIMENTAL STUDY ON EFFECT OF BOUNDARY LAYER ON COMBUSTION MODES IN A SUPERSONIC COMBUSTOR...... 2003 R. Masumoto, H. Yamasaki
HEAT FLUX EVALUATION IN OXYGEN/METHANE THRUST CHAMBERS BY RANS APPROACH...... 2010 B. Betti, E. Martelli, F. Nasuti
CFD ANALYSIS OF CURVED COOLING CHANNEL FLOW AND HEAT TRANSFER IN ROCKET ENGINES ...... 2019 M. Pizzarelli, F. Nasuti, M. Onofri
COMBUSTION AND HEAT TRANSFER MODELING IN REGENERATIVELY COOLED THRUST CHAMBERS (WALL HEAT FLUX VALIDATION) ...... 2033 D. Yu, H. Negishi, N. Yamanishi
CECE: EXPANDING THE ENVELOPE OF DEEP THROTTLING IN LIQUID OXYGEN/LIQUID HYDROGEN ROCKET ENGINES FOR NASA EXPLORATION MISSIONS...... 2045 V. Giuliano, T. Leonard, R. Lyda, T. Kim
NORTHROP GRUMMAN TR202 LOX/GH2 DEEP THROTTLING ENGINE PROJECT STATUS...... 2055 J. Gromski, A. Majamaki, S. Chianese, V. Weinstock, T. Kim
A HIGH-SPEED RESPONSE LOX / LH2 FULL EXPANDER CYCLE ENGINE WITH DEEP THROTTLING CAPABILITY ...... 2066 S. Tokudome, Y. Naruo, H. Mori, T. Yagishita, T. Yamamoto
EFFECTS OF DEEP THROTTLING ON ROCKET ENGINE SYSTEMS...... 2076 T. Kimura, M. Sato, T. Masuoka, T. Kanda, A. Osada
ON THE UNSTEADINESS ASSOCIATED WITH SHOCK-INDUCED SEPARATION IN OVEREXPANDED ROCKET NOZZLES...... 2086 W. Baars, C. Tinney, J. Ruf, A. Brown, D. McDaniels
SIDE LOADS IN DUAL BELL NOZZLES, PART I: PHENOMENOLOGY ...... 2101 R. Stark, C. Nurnberger-Genin
SIDE LOADS IN DUAL BELL NOZZLES, PART II: DESIGN PARAMETERS...... 2111 C. Nurnberger-Genin, R. Stark
DEVELOPMENT AND ON-ORBIT PERFORMANCE OF A PRESSURE REGULATION CONTROL SYSTEM FOR UPPER STAGE...... 2121 C. Clauss, P. Welker, J. Pullano, B. Davis, J. Gambert
PROPELLANT READINESS LEVEL: A METHODOLOGICAL APPROACH TO PROPELLANT CHARACTERIZATION...... 2134 J. Bossard, N. Rhys
RANS AND LES MODELING AND VALIDATION OF WALL-JET FILM COOLING IN A 2-D SLOT...... 2149 A. Voegele, A. Trouve, C. Cadou, A. Marshall
FIRST ORDER BI-PROPELLANT INJECTOR DESIGN AND ANALYSIS FOR SMALL ROCKET ENGINES ...... 2163 D. Morris, J. McKinnon
PROGRAM SUMMARY FOR LOX/METHANE SWIRL-COAXIAL INJECTOR CHARACTERIZATION...... 2176 R. Ikard, R. Frederick Jr., D. Lineberry, M. Moser, M. Balasubramanyam
INJECTOR GEOMETRY EFFECTS ON CRYOGENIC COAXIAL JETS AT SUPERCRITICAL PRESSURES...... 2189 H. Tani, S. Teramoto, T. Nagashima
A NUMERICAL STUDY ON ACOUSTIC DAMPING MECHANISM OF BAFFLED-INJECTORS IN AN ACOUSTIC CHAMBER...... 2205 I. Park, C. Sohn
SIMULATION AND EXPERIMENT RESEARCH FOR A HYDROGEN-RICH/OXYGEN-RICH SHEAR TRICOAXIAL GAS-GAS INJECTOR ...... 2210 G. Cai, M. Li, Y. Gao, P. Jin
NUMERICAL SIMULATION OF DIFFUSION COMBUSTION IN A TURBULENT BOUNDARY LAYER CONSIDERING REACTION PROGRESSION ...... 2225 K. Ishiko, V. Novokzhilov, T. Shimada
NUMERICAL COMPUTATIONS OF PARTICLE-LADEN TURBULENT REACTING FLOWS: A LARGE- EDDY SIMULATION APPROACH...... 2236 M. Ilie
TRANSPORTED PDF MODELING OF TURBULENT NON-PREMIXED JET FLAMES INCLUDING SOOT FORMATION...... 2245 K. Nold, P. Gerlinger, R. Eggels, M. Aigner
SIMULATIONS OF DETONATION BASED CYCLES IN TUBES WITH MULTIPLE OPENINGS...... 2258 W. Stoddard, M. Mihaescu, E. Gutmark
PROPULSION CONTROLS AND DIAGNOSTICS RESEARCH IN SUPPORT OF NASA AERONAUTICS RESEARCH MISSION PROGRAMS...... 2268 S. Garg
MEETING THE REQUIREMENTS OF DISTRIBUTED ENGINE CONTROL VIA DECENTRALIZED, MODULAR SMART SENSING...... 2291 J. Decastro, C. Palmer, A. Behbahani
DISTRIBUTED ENGINE CONTROL DESIGN CONSIDERATIONS...... 2299 W. Merrill, J. Kim, S. Lall, S. Majerus, D. Howe, A. Behbahani
DISTRIBUTED ONBOARD DIAGNOSTIC METHODOLOGY FOR NEXT GENERATION TURBINE ENGINES ...... 2312 S. Zein-Sabatto, M. Bodruzzaman, R. Mgaya, A. Behbahani
APPROACHING SOLID PROPELLANT HETEROGENEITY FOR AGGLOMERATE SIZE PREDICTION ...... 2318 F. Maggi, A. Bandera, L. Luca
AGGREGATION AND INCIPIENT AGGLOMERATION IN METALLIZED SOLID PROPELLANTS AND SOLID FUELS FOR ROCKET PROPULSION ...... 2329 L. Deluca, C. Paravan, A. Reina, E. Marchesi, B. Kosowski
DOUBLE-PULSE SOLID ROCKET MOTOR TECHNOLOGY – APPLICATIONS AND TECHNICAL SOLUTIONS...... 2345 K. Naumann, L. Stadler
THE DOUBLE PULSE MOTOR DEMONSTRATOR MSA ...... 2354 L. Stadler, J. Huber, D. Friedemann, K. Bauer, C. Rienacker, H. Weigand, S. Hoffmann, K. Naumann
THE FLIGHT DEMONSTRATION OF THE DOUBLE PULSE MOTOR DEMONSTRATOR MSA...... 2362 L. Stadler, S. Hoffmann, J. Huber, R. Stingl, K. Naumann
ON THE VISCOUS BIDIRECTIONAL VORTEX. PART 1: LINEAR BELTRAMIAN MOTION ...... 2374 J. Batterson, J. Majdalani
ON THE VISCOUS BIDIRECTIONAL VORTEX. PART 2: NONLINEAR BELTRAMIAN MOTION ...... 2395 J. Batterson, J. Majdalani
ON THE VISCOUS BIDIRECTIONAL VORTEX. PART 3: MULTIPLE MANTLES ...... 2413 J. Batterson, J. Majdalani
FAST TRANSITS TO MARS USING ELECTRIC PROPULSION...... 2433 J. Dankanich, B. Vondra, A. Ilin
VASIMR® PERFORMANCE RESULTS...... 2452 L. Cassady, B. Longmier, C. Olsen, M. Ballenger, G. McCaskill, A. Ilin, M. Carter, T. Glover, J. Squire, F. Diaz, E. Bering III
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON THE THRUST PRODUCTION PROCESS OF MAGNETOPLASMA SAIL...... 2471 I. Funaki, H. Yamakawa, Y. Kajimura, K. Ueno, Y. Oshio, H. Nishida, H. Usui, M. Matsumoto, I. Shinohara
IMPROVEMENTS TO A FLOW SENSOR FOR LIQUID BISMUTH-FED HALL THRUSTERS ...... 2482 K. Bonds, K. Polzin
BACKGROUND GAS PRESSURE EFFECTS IN THE CYLINDRICAL HALL THRUSTER ...... 2489 Y. Raitses, J. Parker, E. Davis, N. Fisch
ELECTRIC PROPULSION MISSION VIABILITY WITHIN THE DISCOVERY CLASS COST CAP...... 2494 J. Dankanich, J. Drexler, S. Oleson
TIME-DOMAIN CHARACTERISTICS OF 0.5 – 8 GHZ PULSED EMISSION FROM HALL THRUSTERS...... 2506 E. Beiting, R. Spector, X. Eapen
SPATIALLY-RESOLVED BEAM CURRENT AND CHARGE-STATE DISTRIBUTIONS FOR THE NEXT ION ENGINE ...... 2514 J. Pollard, K. Diamant, M. Crofton, M. Patterson, G. Soulas
FIRST CUDA FDTD SIMULATION AND EXPERIMENTAL VERIFICATION OF THE MICROWAVE TRANSMISSION AND DISTRIBUTION OF THE MU10 NEUTRALIZER ...... 2532 M. Bodendorfer, H. Koizumi, S. Hosada, K. Nishiyama, H. Kuninaka
PROOF-OF-CONCEPT TESTING OF A SUSTAINED VORTEX-FLOW CONFIGURATION FOR HYBRID ROCKET MOTORS...... 2543 R. Wilkinson, K. Hart, R. Day, I. Coxhill
EXPERIMENTAL INVESTIGATION AND ANALYSIS OF THE SOL-BRID TACTICAL ROCKET MOTOR CONCEPT...... 2553 J. Dennis, S. Shark, J. Villarreal
EXPERIMENTAL PERFORMANCE ANALYSIS OF A TOROIDAL AEROSPIKE NOZZLE INTEGRATED WITH A N2O/HTPB HYBRID ROCKET MOTOR ...... 2581 S. Shark, J. Dennis, J. Villarreal
DEVELOPMENT OF STAGED COMBUSTION AFT-INJECTED HYBRID (SCAIH) PROPULSION AT CESARONI TECHNOLOGY...... 2597 B. Pilon, J. Louwers
OPTIMIZATION OF AIR-BREATHING HYPERSONIC AIRCRAFT DESIGN USING EULER CODES AND GENETIC ALGORITHMS ...... 2613 V. Ahuja, R. Hartfield Jr.
THE NUMERICAL STUDY OF IMPROVING THE PERFORMANCE OF THE OVEREXPANDED SERN BY USING SJA ...... 2636 J. Xu, J. Sha, J. Mo, Y. Yu, K. Zhang
CONTINUED INVESTIGATION OF SHORT CONTACT TIME REACTORS FOR REGENERATIVELY- COOLED HYPERSONIC VEHICLES ...... 2643 J. Leylegian, W. Chinitz, G. Benel, M. Castaldi
LARGE-EDDY SIMULATION OF SUPERSONIC FILM COOLING...... 2658 M. Konopka, M. Meinke, W. Schroder
TRANSPIRATION COOLING WITH SUPERSONIC FLOWS AND FOREIGN GAS INJECTION ...... 2672 T. Langener, J. Wolfersdorf, M. Kuhn, J. Steelant
MARS EARTH RETURN VEHICLE (MERV) PROPULSION OPTIONS...... 2685 S. Oleson, M. McGuire, L. Burke, J. Fincannon, T. Colozza, J. Fittje, M. Martini, T. Packard, J. Hemminger, J. Gyekenyesi
PROPULSION MODULE: A COMPARISON OF TECHNICAL AND ECONOMICAL APPROACHES, THEIR RESPECTIVE MERITS, AND INFLUENCE ON SYSTEM LEVEL...... 2741 M. Lange, M. Holzwarth
AN ANALYSIS OF ROCKET PROPULSION TESTING COSTS ...... 2747 C. Ramirez, S. Rahman
CAPTURING AND RECYCLING OF XENON FROM A CRYOPUMPED VACUUM CHAMBER ...... 2760 M. Swaitek
PERFORMANCE AND STABILITY ANALYSES OF ROCKET COMBUSTION DEVICES USING LIQUID OXYGEN/LIQUID METHANE PROPELLANTS...... 2768 J. Hulka, G. Jones
NONLINEAR LIQUID ROCKET COMBUSTION INSTABILITY BEHAVIOR USING UCDS™ PROCESS ...... 2796 E. Jacob, G. Flandro, P. Gloyer, J. French
VOLUME 4
AXIALLY TRAVELING WAVES IN POROUS TUBES WITH ARBITRARY CROSSFLOW VELOCITY...... 2806 T. Jankowski, J. Majdalani
EXPERIMENTAL AND NUMERICAL COMBUSTION INSTABILITY MODES IN ASYMMETRIC BAFFLED CHAMBERS ...... 2824 J. Quinlan, O. Bibik, B. Zian
EFFECT OF COMBINED HUB/BLADE BAFFLES ON THE COMBUSTION STABILITY OF A LIQUID ROCKET ENGINE...... 2835 A. Kirkpatrick, T. Hinerman
FUEL TRADE STUDY FOR A NANOSAT LAUNCH VEHICLE UPPER STAGE ...... 2843 A. Delamata, E. Besnard, C. Bostwick
GENERALIZED MONO/BI-PROPELLANT PROPULSION SYSTEM FOR MICROSATELLITE BASED ON NON-TOXIC PROPELLANT TECHNOLOGY...... 2858 N. Suzuki, H. Sahara
PLASMA-ASSISTED COMBUSTION OF N2O/ETHANOL PROPELLANT FOR SPACE PROPULSION ...... 2863 A. Kakami, T. Egawa, N. Yamamoto, T. Tachibana
EFFECT OF CATALYST LOADING CONDITION TO PERFORMANCE OF HYDROGEN PEROXIDE MICRO THRUSTER...... 2870 J. Lee, S. An, S. Kwon
A NOVEL EXPERIMENTAL FACILITY FOR IMPINGING JET INJECTOR FLOW STUDIES...... 2876 J. Mallory, P. Sojka
HAZARD ASSESSMENT OF OXYGEN PROPELLANT SYSTEMS AT UAHUNTSVILLE PROPULSION RESEARCH CENTER ...... 2882 H. Mulkey, D. Lineberry, M. Moser
LIQUID JET DYNAMICS AND PRIMARY BREAKUP CHARACTERISTICS AT NEAR-FIELD OF COAXIAL TYPE INJECTOR...... 2894 C. Inoue, T. Watanabe, T. Himeno, S. Uzawa
EXPERIMENTAL STUDY ON THE INTERNAL FLOW CHARACTERISTICS FOR RECESS LENGTH IN A SWIRL COAXIAL INJECTOR...... 2906 S. Kim, J. Yoon, Y. Yoon
DETAILS OF SIDE LOAD TEST DATA AND ANALYSIS FOR A TRUNCATED IDEAL CONTOUR NOZZLE AND A PARABOLIC CONTOUR NOZZLE...... 2913 J. Ruf, D. McDaniels, A. Brown
INVESTIGATION OF EFFECT OF GROUND DOWNSTREAM OF OVEREXPANDED DUAL-BELL NOZZLE DURING VERTICAL TAKEOFF AND LANDING ...... 2965 K. Yonezawa, D. Proschchanka, H. Koga, H. Tsukuda, Y. Tsujimoto, T. Kimura, K. Yokota
CONTROL OF OPERATION MODE TRANSITION IN DUAL-BELL NOZZLE WITH FILM COOLING ...... 2980 D. Proshchanka, K. Yonezawa, H. Koga, H. Tsukuda, Y. Tsujimoto, T. Kimura, A. Pasini
ENRICHMENT ZONING OPTIONS FOR THE SMALL NUCLEAR ROCKET ENGINE (SNRE) ...... 2996 B. Schnitzler, S. Borowski
HUMAN EXPLORATION USING REAL-TIME ROBOTIC OPERATIONS (HERRO) -CREW TELEROBOTIC CONTROL VEHICLE (CTCV) DESIGN...... 3005 S. Oleson, M. McGuire, L. Burke, D. Chato, J. Fincannon, T. Colozza, J. Fittje, M. Martini, T. Packard, D. McCurdy, J. Gyekenyesi
NTR DEVELOPMENT STRATEGY AND KEY ACTIVITIES SUPPORTING NASA HUMAN MARS MISSIONS IN THE EARLY-2030 TIMEFRAME ...... 3060 S. Borowski, B. Schnitzler
SOLAR ELECTRIC AND NUCLEAR THERMAL PROPULSION ARCHITECTURES FOR HUMAN MARS MISSIONS BEGINNING IN 2033 ...... 3066 B. Donahue
ON SHEAR-THINNING GEL PROPELLANTS WITH METAL POWDERS ...... 3085 V. Chernov, B. Natan
ATOMIZATION OF NON-NEWTONIAN FLUIDS WITH AN IMPINGING JET INJECTOR: INFLUENCE OF VISCOELASTICITY ON HINDERING DROPLETS FORMATION ...... 3096 M. Negri, H. Ciezki
SECONDARY ATOMIZATION OF ELASTIC NON-NEWTONIAN LIQUID DROPS...... 3107 S. Snyder, N. Arockiam, P. Sojka
A GRAPHICAL SPRAY ANALYSIS METHOD FOR GEL SPRAY CHARACTERIZATION ...... 3118 J. McCabe, M. Coil
EXTENT AND IMPACTS OF HYDROCARBON FUEL COMPOSITIONAL VARIABILITY FOR AEROSPACE PROPULSION SYSTEMS ...... 3136 M. Billingsley, T. Edwards, L. Shafer, T. Bruno
UPDATING OUR UNDERSTANDING OF JP-10 DECOMPOSITION CHEMISTRY: A DETAILED JP-10 COMBUSTION MECHANISM CONSTRUCTED USING RMG, AN AUTOMATIC REACTION MECHAN...... 3151 G. Magoon, W. Green, O. Oluwole, H. Wong, S. Albo, D. Lewis
DYNAMIC SPATIAL AND TEMPORAL ALLOCATION OF REDUCED CHEMICAL KINETICS MODELS IN COMBUSTION COMPUTATIONAL FLUID DYNAMICS SIMULATIONS ...... 3168 O. Oluwole, H. Wong, R. Miake-Lye, W. Green Jr.
SMALL-SCALE PLANAR NITROUS OXIDE MONOPROPELLANT THRUSTER FOR “GREEN” PROPULSION AND POWER GENERATION...... 3176 Y. Scherson, K. Lohner, B. Cantwell, T. Kenny
ACTIVE RETRACTABLE SEALS FOR HIGH-EFFICIENCY STEAM TURBINES ...... 3185 B. Roy, N. Turnquist, X. Zheng, B. Couture, C. Jones
EXPERIMENTAL RESULTS FROM A SENSOR BRUSH SEAL ...... 3190 E. Ruggiero
EVALUATION OF PRESSURE-STIFFNESS COUPLING IN BRUSH SEALS ...... 3201 S. Aksoy, M. Aksit
IMPROVED MOISTURE PERFORMANCE OF ANTIOXIDANT IMPREGNANT IN GRAPHITE SEALS, BUSHINGS, AND STRUCTURES...... 3210 W. Hambek, R. Sheppard, C. Extrand, M. Gonzales, T. Scoggins
USING HIGH TEMPERATURE ELECTRONICS FOR DISTRIBUTEDCONTROLS OF TURBINE ENGINES ...... 3219 M. Willett, M. Ward, A. Behbahani
DECENTRALIZED ADAPTIVE CONTROL OF A TURBOFAN SYSTEM WITH PARTIAL COMMUNICATION ...... 3232 M. Pakmehr, N. Fitzgerald, G. Kiwada, J. Paduano, E. Feron, A. Behbahani
INNOVATIVE SENSOR WITH PHYSICS-BASED DEFECT SEVERITYESTIMATION TECHNIQUE ...... 3248 C. Larsen, S. Shelley
DISTRIBUTED, INTEGRATED PHM AND CONTROL VIA SMART ENGINEACCESSORIES FOR FUTURE MODERN AIRCRAFT...... 3257 M. Watson, J. Sheldon, A. Behbahani
PARAMETRIC EVALUATION OF SOLID ROCKET MOTOR INTERNAL BALLISTICS ...... 3270 D. Greatrix
STUDIES ON INTERNAL BALLISTICS OF DUAL-THRUST MOTORS FORNOZZLELESS PROPULSION...... 3281 V. Kumar, B. Raghunandan, T. Kawakami
MODELING MACH NUMBER AND TEMPERATURE DISTRIBUTIONS IN SUPERSONIC NOZZLE FLOW...... 3291 J. Majdalani, B. Maicke
NUMERICAL SIMULATION OF GRAPHITE NOZZLE EROSION WITH PARAMETRIC ANALYSIS ...... 3301 R. Acharya, K. Kuo
STUDY ON INFRARED SIGNATURE OF SOLID ROCKET MOTOR AFTERBURNING EXHAUST PLUME...... 3319 W. Wang, Z. Wei, Q. Zhang, J. Tang, N. Wang
HIGHLY RELIABLE DESIGN APPROACHES FOR NEXT BOOSTER ENGINE LE-X...... 3325 N. Kumada, A. Ogawara, H. Manako, T. Onga, H. Sunakawa, A. Kurosu, N. IIzuka, K. Noda, K. Okita
DYNAMIC CHARACTERISTICS OF A FLUIDIC VALVE FOR DIVERT ANDATTITUDE CONTROL SYSTEM...... 3334 J. Heo, K. Yoo, Y. Lee, H. Sung, S. Cho, Y. Jeon
THERMAL STRESS ANALYSIS OF CERAMIC PELLETS FOR CATALYSIS...... 3348 A. Pasini, L. Torre, L. Romeo, A. Cervone, A. D'Agostino
LOW-THRUST MISSION DESIGN AND APPLICATION...... 3360 J. Dankanich
IN-SPACE PROPULSION HIGH VOLTAGE HALL ACCELERATOR DEVELOPMENT PROJECT OVERVIEW...... 3379 H. Kamhawi, D. Manzella, L. Pinero, T. Haag, W. Huang
MASS FLOW CONTROL IN A MAGNESIUM HALL-EFFECT THRUSTER...... 3390 M. Hopkins, J. Makela, R. Washeleski, L. King
HAYABUSA'S WAY BACK TO EARTH BY MICROWAVE DISCHARGE ION ENGINES...... 3400 K. Nishiyama, S. Hosoda, H. Koizumi, Y. Shimizu, I. Funaki, H. Kuninaka, M. Bodendorfer, J. Kawaguchi, D. Nakata
PARTICLE-IN-CELL MODEL OF THE NEXT ION ENGINE AT THREE THROTTLING CONDITIONS...... 3412 M. Jonell, J. Menart, S. Mahalingam
RF CABLE HEATING EFFECTS ON A MICRONEWTON-SCALE TORSIONAL THRUST STAND...... 3426 S. Williams, I. Hrbud
ACTIVE COMBUSTION CONTROL SYSTEM RIG TESTING...... 3439 J. Goeke, N. Overman
AN EXPERIMENTAL INVESTIGATION OF ACOUSTIC AND COMBUSTIONWAVE INTERACTION CHARACTERISTICS IN DUMP COMBUSTOR ...... 3450 M. Kim, J. Lee, S. Park, J. Yoon, Y. Yoon
HEAT TRANSFER AND FRICTION IN HIGH ASPECT RATIO INTERNAL COOLING CHANNELS MACHINED WITH VARIOUS TECHNIQUES ...... 3461 L. Tran, C. Slabaugh, J. Kapat, M. Ricklick
THE INFLUENCE OF DISCRETIZATION SCHEME ON LARGE EDDYSIMULATIONS OF DISCRETE FILM COOLING HOLES ...... 3478 P. Johnson, C. Nguyen, S. Ho, J. Kapat
COMPARISON OF HEAT TRANSFER AND THERMAL PERFORMANCE OFA DOUBLE WALL COOLING SCHEME AT LARGE IMPINGEMENT HEIGHTS...... 3495 R. Claretti, M. Ricklick, J. Kapat
PRELIMINARY PYROLYSIS AND COMBUSTION STUDY FOR THE HYBRIDPROPULSION...... 3510 N. Gascoin, P. Gillard
SIMULATION CODE FOR HYBRID ROCKET COMBUSTION...... 3522 G. Gariani, F. Maggi, L. Galfetti
REGRESSION MODELING OF PARAFFIN-BASED HYBRID ROCKET FUELS FOR INTERNAL BALLISTICS SIMULATION...... 3535 Y. Funami, V. Novozhilov, I. Nakagawa, T. Shimada
PREDICTION OF TIME VARIATION OF BALLISTIC PARAMETERSFOR A SWIRLING-OXIDIZER- FLOW-TYPE HYBRID ROCKET ENGINE USING BURNING DATA...... 3545 N. Shiraishi, S. Yuasa
CFD ENHANCEMENTS FOR SUPERSONIC COMBUSTION SIMULATION WITH VULCAN...... 3552 F. Ladeinde, K. Alabi, T. Ladeinde, D. Davis, M. Satchell, R. Baurle
NOVEL VALVING TECHNIQUE FOR PULSE DETONATION ENGINES...... 3602 E. Anderson, J. Hoke, F. Schauer
NUMERICAL INVESTIGATION OF ROTATING DETONATION ENGINES...... 3608 D. Schwer, K. Kailasanath
DEVELOPMENT OF A HYDROGEN-FUELED PULSE DETONATION COMBUSTOR FOR 1 KW-CLASS MICRO GAS TURBINE ...... 3623 T. Sakurai, S. Yuasa
EXPERIMENTAL STUDIES OF THE UNSTEADY EJECTOR MODE OF A PULSE DETONATION ROCKET- BASED COMBINED CYCLE ENGINE ...... 3631 N. Mercurio, S. Pal, R. Woodward, R. Santoro
PERFORMANCE RESULTS FOR THE ADVANCED MATERIALS BIPROPELLANT ROCKET (AMBR) ENGINE ...... 3647 S. Henderson, L. Liou, L. Alexander, J. Dankanich
PERFORMANCE IMPROVEMENTS IN SMALL EARTH STORABLE ROCKET ENGINES- AN ERA OF APPROACHING THE THEORETICAL ...... 3658 C. Stechman, S. Harper
DEVELOPMENT OF A SUPERSONIC FILM COOLING TEST FACILITY...... 3669 D. Maqbool, K. Dellimoore, C. Cadou
TMF TEST BASED VALIDATION OF NUMERICAL METHODS FOR THEANALYSIS OF HEAT-LOADED WALLS...... 3683 A. Gernoth, M. Wurdak, J. Riccius, S. Schlechtriem, D. Wiedmann, W. Schwarz, L. Brummer
NUMERICAL INVESTIGATION OF SUPERCRITICAL COOLANT FLOW IN LIQUID ROCKET ENGINE ...... 3695 H. Negishi, D. Yu, N. Yamanishi, Y. Ohnishi
PROPELLANT SLOSHING PARAMETER EXTRACTION FROM CFD ANALYSIS ...... 3715 H. Yang, J. Peupeot
HYBRID FINITE ELEMENT/MOLECULAR DYNAMICS SIMULATIONS OFALUMINUM PARTICLE WALL COLLISIONS...... 3732 M. Micci, M. Crofton
MODELING OF CRYOGENIC SLOSHING INCLUDING HEAT AND MASS TRANSFER...... 3738 A. Foreest
VOLUME 5
INFLUENCE OF PUMP CAVITATION PROCESS ON POGO DIAGNOSIS FORTHE A5E/CA UPPER STAGE...... 3758 S. Muller, F. Breviere, A. Kernilis, N. Lemoine
SCALING A SINGLE ELEMENT ATMOSPHERIC COMBUSTOR...... 3776 B. Sweeney, D. Lineberry, R. Frederick Jr.
CHARACTERIZATION OF A SINGLE SWIRL-COAXIAL INJECTOR IN A SUB-SCALE COMBUSTOR...... 3795 J. Brooks, D. Lineberry, R. Frederick Jr.
CHARACTERIZATION OF AN UNSTABLE ROCKET COMBUSTOR WITH HE ADDITION...... 3811 M. Wierman, N. Nugent, W. Anderson
REACTION DYNAMICS AND PROBABILITY STUDY OF ALUMINUM-VITON-ACETONE DROPLETS...... 3821 S. Datta, M. Pantoya, B. Dikici, S. Ekwaro
COMBUSTION WAVE STRUCTURE OF HYDROXYLAMMONIUM NITRATEAQUEOUS SOLUTIONS...... 3834 T. Katsumi, K. Hori, R. Matsuda, T. Inoue
HYPERGOLIC IGNITION OF A GELLED IONIC LIQUID FUEL ...... 3845 M. Coil
ASPECTS OF MONOMETHYLHYDRAZINE AND RED FUMING NITRIC ACID IGNITION ...... 3856 T. Kubal, E. Dambach, S. Son, W. Anderson, T. Pourpoint
NUMERICAL STUDY OF EROSIVE BURNING IN SOLID PROPELLANTS...... 3874 V. Topalian, J. Zhang, T. Jackson
EROSIVE BURNING OF TWO-DIMENSIONAL PACKS OFAP/BINDER SOLID PROPELLANTS USING SHEAR MODEL BASED ON MULTISCALE ANALYSIS ...... 3883 J. Zhang, T. Jackson
DETAILED CHARACTERIZATION OF AL/ICE PROPELLANTS ...... 3897 T. Pourpint, T. Sippel, C. Zaseck, T. Wood, S. Son, G. Risha, R. Yetter
AN EXPERIMENTAL INVESTIGATION OF LEAK RATEPERFORMANCE OF A SUBSCALE CANDIDATE ELASTOMER DOCKING SPACE SEAL...... 3908 N. Garafolo, C. Daniels
COMPRESSION FORCE RESPONSE AND LEAK RATE QUANTIFLCATION OF CANDIDATE STATIC SILICONE SPACE SEALS...... 3917 M. Bastrzyk, N. Garafolo, C. Daniels
PIONEERS IN PROPULSION—A HISTORY OF CSD, PRATT & WHITNEY’S SOLID ROCKET COMPANY...... 3926 C. Chase
ARES I-X: FIRST FLIGHT OF A NEW GENERATION ...... 3959 S. Davis, B. Askins
FLOW STRUCTURES OF GASEOUS JET INJECTED INTO LIQUID FOR UNDERWATER PROPULSION ...... 3970 J. Tang, S. Li, N. Wang, Y. Wei, W. Shyy
EROSIVE BURNING: LANDSBAUM REVISITED...... 3984 R. Glick
TOWARDS A PREDICTIVE PROPELLANT BURNING RATE MODEL BASED ON HIGH-FIDELITY NUMERICAL CALCULATIONS ...... 3995 M. Gross
APPLICATION OF CONTINUATION TECHNIQUES TO PRESSURE AND INITIAL TEMPERATURE SENSITIVITY COEFFICIENT CALCULATIONS IN AMMONIUM PERCHLORATE FLAMES ...... 4008 S. Rahman, V. Giovangigli, V. Borie
DESIGN, COMMISSIONING AND CONTROL SYSTEM OF A HYBRID ROCKET TEST CELL ...... 4027 R. Wilkinson, K. Hart, R. Day, I. Coxhill
A STUDENT APPROACH TO ROCKET DESIGN...... 4038 K. Collins, A. Burt, M. Moser
MANEUVERING AND GRAVITY OFFSET FLIGHT CONTROLS FOR AN EXTRATERRESTRIAL SURFACE LANDING RESEARCH VEHICLE ...... 4050 M. Schaefermeyer, S. Whitmore, C. Wright
DEVELOPMENT OF COMPACT HIGH-POWER LASER SYSTEM FOR LASER-ELECTRIC HYBRID PROPULSION SYSTEM ...... 4091 H. Horisawa, T. Shinohara, K. Tei
CURRENT NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF THEHYBRID DC-RF THRUSTER TIHTUS ...... 4102 U. Bauder, S. Lohle, D. Petkow, G. Herdrich, S. Fasoulas, M. Fertig, M. Auweter-Kurtz
THRUST GENERATION PHENOMENA THROUGH LOW-POWER CW LASER–METAL INTERACTION FOR ONBOARD SPACE PROPULSION SYSTEMS...... 4118 H. Horisawa, S. Sumida, H. Yonamine, I. Funaki
OPTIMAL FREQUENCY FOR PLASMA HEATING WITH A SINGLE ELECTROSTATIC WAVE...... 4124 B. Jorns, E. Choueiri
PREDICTING HALL THRUSTER OPEARTIONAL LIFETIME USING A KINETIC PLASMA MODEL AND A MOLECULAR DYNAMICS SIMULATION ...... 4133 Y. Choi, S. Mahalingam, J. Loverich, P. Messmer
MAGNETIC SHIELDING OF THE ACCELERATION CHANNEL WALLS IN A LONG-LIFE HALL THRUSTER ...... 4167 I. Mikellides, I. Katz, R. Hofer, D. Goebel, K. Grys, A. Mathers
DYNAMIC ELECTRIC FIELD CALCULATIONS USING A FULLY KINETICION THRUSTER DISCHARGE CHAMBER MODEL ...... 4192 S. Mahalingam, Y. Choi, J. Loverich, P. Stoltz, M. Jonell, J. Menart
CURRENT STATUSES OF GRAPHITE HOLLOW CATHODE LIFE TESTS ...... 4206 Y. Ohkawa, Y. Hayakawa, H. Yoshida, K. Miyazaki, S. Kitamura, H. Nagano, K. Kajiwara
VALIDATION OF AN ION-THRUSTER GRID THERMAL MODEL WITHEXPERIMENTS...... 4214 Y. Hayakawa, H. Yoshida, K. Miyazaki, Y. Ohkawa, H. Nagano, S. Kitamura
NUMERICAL ANALYSIS OF A MICRO ION THRUSTER USING PIC/MCC MODEL...... 4224 Y. Takao, K. Eriguchi, K. Ono
FLOW MEASUREMENTS USING PARTICLE IMAGE VELOCIMETRY IN THE ULTRA COMPACT COMBUSTOR...... 4233 L. Thomas, R. Branam
INVESTIGATION OF DISTRIBUTED COMBUSTION FOR GAS TURBINEAPPLICATION: REVERSE FLOW CONFIGURATION...... 4248 V. Arghode, A. Gupta
TEMPERATURE MEASUREMENTS OF POROUS MEDIA FOR TRANSPIRATION STUDIES ...... 4264 G. Natsui, M. Ricklick, C. Nguyen, J. Kapat
DEVELOPMENT OF A TRANSONICWIND TUNNEL TO INVESTIGATE ENGINE BYPASS FLOW HEAT EXCHANGERS...... 4274 L. Villafane, G. Paniagua, J. Desset, D. Bajusz, S. Hiernaux
HEAT TRANSFER AND FRICTION AUGMENTATION IN A NARROW RECTANGULAR DUCT WITH RIBS APPLIED TO ONE WALL ...... 4289 C. Slabaugh, M. Valentino, M. Ricklick, J. Kapat
A STUDY OF HEAT TRANSFER AUGMENTATION IN A RECTANGULAR CHANNEL WITH DIMPLES APPLIED TO ONE WALL...... 4306 C. Slabaugh, L. Tran, J. Kapat
OPTIMIZATION OF A HYBRID ROCKET UPPER STAGE WITH ELECTRIC PUMP FEED SYSTEM ...... 4335 L. Casalino, D. Pastrone
NON-LINEAR COMBUSTION AND LES ANALYSIS WITH WALL BLOWING IN HYBRID ROCKET ...... 4346 B. Kim, Y. Na, C. Lee
DUAL MODE SCRAMJET DESIGN TO ACHIEVE IMPROVED OPERATIONALSTABILITY ...... 4358 S. Torrez, D. Dalle, J. Driscoll
REDUCED-ORDER MODELING OF REACTING SUPERSONIC FLOWS INSCRAMJET NOZZLES...... 4370 D. Dalle, S. Torrez, J. Driscoll
MIXING CONTROL BY WALL FLUSH-MOUNT INJECTORS IN DUAL-MODE COMBUSTOR ...... 4389 S. Tomioka, M. Izumikawa, N. Sakuranaka, H. Shibata, H. Yamasaki, T. Kobayashi, A. Matsuo
NUMERICAL STUDY ON AIRFLOW/JET MIXING ENHANCEMENT BYPSEUDO-SHOCK WAVE SYSTEM...... 4399 T. Kobayashi, A. Matsuo, S. Tomioka, M. Izumikawa
AN IMPROVED LOBED STRUT INJECTOR CONCEPT FOR SUPERSONIC COMBUSTION ...... 4409 B. Rust, P. Gerlinger, M. Aigner
ANALYTICAL AND EXPERIMENTAL EVALUATION OF AERODYNAMICTHRUST VECTORING ON AN AEROSPIKE NOZZLE...... 4420 S. Eilers, M. Wilson, S. Whitmore
HYDROGEN MICROTHRUSTERS BASED ON HYDROGEN STORAGE MATERIALS ...... 4444 F. Nasuti, B. Betti, M. Balucani
CONSTANT MOMENTUM EXCHANGE BETWEEN MICROSPACECRAFT USING LIQUID DROPLET THRUSTERS...... 4453 T. Joslyn, A. Ketsdever
ANALYSIS OF INTERACTING, UNDER-EXPANDED, RAREFIED JETS ...... 4462 W. Li, F. Ladeinde
THE J-2X UPPER STAGE ENGINE: FROM DESIGN TO HARDWARE...... 4490 T. Byrd
PROGRESS OF THE VINCI ENGINE SYSTEM DEVELOPMENT ...... 4504 P. Alliot, C. Fiorentino, E. Edeline, L. Appolloni
HIGH THRUST ENGINE DEMONSTRATIONS ...... 4515 J. Lonchard, I. Jeaugey, J. Montheillet, F. Lassoudiere, G. Dantu, A. Beaurain, P. Alliot
ANALYSIS OF FLAME DEFLECTOR SPRAY NOZZLES IN ROCKET ENGINETEST STANDS...... 4524 J. Sachdev, V. Ahuja, A. Hosangadi, D. Allgood
EFFECTS COOLING CHANNEL CURVATURE ON COOLANT SECONDARYFLOW AND HEAT TRANSFER...... 4534 J. Divalentin, M. Naraghi
MODELLING OF STRATI CATION IN COOLING CHANNELS AND ITSIMPLEMENTATION IN A TRANSIENT SYSTEM ANALYSIS TOOL ...... 4549 F. Matteo, M. Rosa, M. Pizzarelli, M. Onofri
A CHALLENGE OF PREDICTING THERMO-MECHANICAL BEHAVIOR OF ABLATING SIFRP WITH FINITE ELEMENT ANALYSIS...... 4564 Y. Matsuura, K. Hirai
ENHANCED NUMERICAL MODELING IN SIMULATION OF A GENERIC PROPELLANT TANK SLOSH BAFFLE ...... 4589 S. Chintalapati, J. Faure, R. Zhou, M. Vergalla, D. Kirk, H. Gutierrez
EXPERIMENTAL METHODOLOGY AND NUMERICAL TECHNIQUE FOR 6-DOF TANK SLOSH DYNAMICS ...... 4601 R. Zhou, M. Vergalla, D. Kirk, H. Gutierrez
TIME FREQUENCY ANALYSIS OF SPACECRAFT PROPELLANT TANK SPINNING SLOSH ...... 4615 S. Green, R. Burkey, J. Sudermann
HEAT EXCHANGE AND PRESSURE DROP ENHANCED BY VIOLENT SLOSHING...... 4624 T. Himeno, D. Sugimori, S. Uzawa, T. Watanabe, S. Nonaka
SIMULATED ALTITUDE LIQUID ROCKET TESTING AT THE USAF AEDC: ATLAS/MERCURY, TITAN/GEMINI, SATURN/APOLLO, SPACE SHUTTLE, ISS...... 4653 N. Dougherty
THERMAL AND CATALYTIC DECOMPOSITION OF H2O2-IONIC LIQUID MONOPROPELLANT MIXTURES ON MONOLITH-BASED CATALYSTS ...... 4701 R. Amrousse, R. Brahmi, Y. Batonneau, C. Kappenstein
VOLUME 6
IGNITION OF ADVANCED HYPERGOLIC PROPELLANTS...... 4707 E. Dambach, K. Cho, T. Pourpoint, S. Heister
DECOMPOSITION OF HYDROGEN PEROXIDE: INFLUENCE OF THE SHAPEOF CATALYST SUPPORT ...... 4719 K. Farhat, Y. Batonneau, C. Kappenstein, M. Theron
TEMPERATURE AND ATOMIC OXYGEN EFFECTS ON HELIUM LEAK RATES OF A CANDIDATE MAIN INTERFACE SEAL ...... 4726 N. Penney, J. Wasowski, C. Daniels
FULL-SCALE SYSTEM FOR QUANTIFYING LOADS AND LEAK RATES OFSEALS FOR SPACE APPLICATIONS...... 4733 P. Dunlap Jr., B. Steinetz, C. Daniels, J. Wasowksi, M. Robbie, A. Erker, G. Drlik, J. Mayer
TDLAS-BASED MEASUREMENTS OF TEMPERATURE, PRESSURE, AND VELOCITY IN THE ISOLATOR OF AN AXISYMMETRIC SCRAMJET...... 4753 M. Brown, D. Barone, T. Barhorst, D. Eklund, M. Gruber, T. Mathur, R. Milligan
TURBINE ENGINE TEMPERATURE PATTERN FACTOR CONTROL SYSTEMBASED ON FUEL MODULATION AND PASSIVE OPTICAL SENSORS ...... 4760 J. Cline, J. Lee, E. Perillo, N. Goldstein, S. Swenson-Dodge, J. Ols, S. Kramer
PIV STUDY AND NUMERICAL SIMULATION OF THE UNSTEADYFLOWFIELD OF OVEREXPANDED SUPERSONIC IMPINGING JET AT MA=3 ...... 4772 J. Xu, C. Lin, K. Liu, J. Mo
PIV EXPERIMENTAL AND NUMERICAL INVESTIGATION OFSUPERSONIC INLET AND ISOLATOR...... 4780 J. Ma, J. Xu, J. Mo, R. Gu, K. Zhang
AXIAL WAVES IN SIMULATED SOLID ROCKET MOTORS...... 4790 N. Zgheib, J. Majdalani
UCDS NOZZLE ACOUSTIC DYNAMICS AND STABILITY MODELING ...... 4800 J. French, G. Flandro, P. Gloyer, E. Jacob
CONCURRENT CHARACTERIZATION OF MEAN BURNING RATE AND MASS AND FLAME TEMPERATURE RESPONSE FUNCTIONS...... 4812 R. Glick
NUMERICAL SIMULATIONS OF ACOUSTIC RESONANCE OF SOLID ROCKET MOTOR...... 4821 V. Ferretti, B. Favini, E. Cavallini, F. Serraglia, M. Giacinto
OVERVIEW OF CNES STUDIES ON RELIABILITY METHODS FOR SPACEEXPLOSIVE DEVICES...... 4839 K. Pfaab
NEW IM ISSUE ON NAVAL PLATFORMS: SOLID ROCKET MOTOR (SRM) PNEUMATIC EXPLOSION RISK. EFFECTS PREDICTION METHODOLOGY ...... 4850 N. Duval, E. Faucher, Y. Garcia
THE OPERATING CHARACTERISTICS OF A DUCTED ROCKET IN THE MARS ATMOSPHERE ...... 4863 M. Ushijima, H. Hara, A. Muramatsu, T. Kuwahara
LARGE SPACE SOLID PROPULSION IN FRENCH ‘AQUITAINE’HERITAGE AND PROJECTS ...... 4870 D. Boury
A FOUNDATIONAL HEAVY LIFT LAUNCH VEHICLE ENABLING DEEP SPACE MISSIONS...... 4882 W. Rothschild, T. Talay, E. Henderson
PREDICTION OF THERMO-PHYSICAL PROPERTIES OF ENERGETICMATERIALS BY SIMILARITY TO INERT SUBSTANCES ...... 4898 L. Yang
MODELING THE ENERGY RELEASE CHARACTERISTICS OF THPP BASEDINITIATORS ...... 4921 B. Poulsen, K. Rink
STUDIES ON SPACE DEBRIS TRACKING AND ELIMINATION ...... 4934 A. Molayath, Y. Khan, V. Kumar
A MARS UTILITY VEHICLE DESIGN WITH INCORPORATED REGENERATIVE FUEL CELL TECHNOLOGY AND IN-SITU RESOURCE UTILIZATION ...... 4940 M. Snyder, E. Joyce, J. Longo, B. Justice
ARCHIVING PROPULSION LABORATORY DATA ...... 4952 A. Hiatt, R. Ikard, R. Frederick Jr.
EXPERIMENTAL PULSATOR CHARACTERIZATION FOR LIQUID INJECTORRESEARCH ...... 4964 M. Wilson, D. Lineberry, M. Moser
PRELIMINARY STUDY ON ELECTRODELESS MAGNETO-PLASMA-DYNAMIC THRUSTER USING A HELICON PLASMA SOURCE ...... 4974 H. Nishida, S. Shinohara, T. Tanikawa, T. Hada, I. Funaki, T. Matsuoka, K. Shamrai, T. Motomura
LOW FREQUENCY OSCILLATIONS IN THE DIVERGING CUSPED-FIELD THRUSTER ...... 4985 S. Gildea, T. Matlock, P. Lozano, M. Martinez-Sanchez
MAIN BELT ASTEROID SAMPLE RETURN MISSION DESIGN ...... 5010 J. Dankanich, D. Landau, M. Martini, S. Oleson, A. Rivkin
SPACE SIMULATION TESTING OF THE HELICON DOUBLE LAYER THRUSTER PROTOTYPE...... 5027 M. West, C. Charles, R. Boswell
THRUST STAND FOR VERTICALLY ORIENTED ELECTRIC PROPULSION PERFORMANCE EVALUATION ...... 5044 T. Moeller, K. Polzin
PERFORMANCE CHARACTERIZATION OF THE MICRO-CATHODE ARC THRUSTER AND PROPULSION SYSTEM FOR SPACE APPLICATIONS...... 5055 T. Zhuang, A. Shashurin, S. Haque, M. Keidar
RE-GENERABLE FIELD EMISSION CATHODES PART I: SURFACE MORPHOLOGY OF IN2O3 EMITTER APEX ...... 5063 J. Makela, R. Washeleski, L. King
ON THE VALIDATION OF POROUS NICKEL AS SUBSTRATE MATERIAL FOR ELECTROSPRAY ION PROPULSION...... 5077 D. Courtney, H. Li, P. Maqueo, T. Fedkiw, P. Lozano
MACH 2 SIMULATIONS OF EXOTHERMIC PROPELLANTS IN A MICRO-LASER ABLATION PLASMA THRUSTER ...... 5091 R. Thompson, T. Moeller
GEOMETRY EFFECTS ON THE PERFORMANCE OF CYLINDRICAL-CONICAL (CYLICONE) PLASMA THRUSTERS...... 5102 S. Jaisankar, T. Sheshadri
SCALING OF EFFICIENCY WITH APPLIED MAGNETIC FIELD IN MANGNETOPLASMADYNAMIC THRUSTERS...... 5110 D. Lev, E. Choueiri
INFRARED ASSESSMENT OF OVERALL EFFECTIVENESS OF A MODERN TURBINE VANE COOLING SCHEME...... 5120 J. Johnson, P. King, J. Clark, A. Lethander, K. Lyons, M. Ooten, P. Johnson, J. Downs
THREE-DIMENSIONAL VISCOUS CFD PREDICTIONS OF VANE-ONLY CONFIGURATION OF A FULL- SCALE EXPERIMENTAL TURBINE RIG...... 5133 J. Johnson, P. King, J. Clark, R. Anthony, P. Koch, M. Ooten, J. Finnegan, M. Kobelak, P. Johnson, F. Huber
REGRESSION RATE CHARACTERISTICS AND BURNING MECHANISM OF SOME HYBRID ROCKET FUELS ...... 5145 S. Hikone, S. Maruyama, T. Isiguro, I. Nakagawa
EFFECT OF PARAFFIN-LDPE BLENDED FUEL ON THE HYBRID ROCKET MOTOR...... 5152 S. Kim, J. Lee, H. Moon, H. Sung, J. Kim, J. Cho
A STUDY ON BURNING RATE WITH MASS TRANSFER NUMBER (B NUMBER) OF SOLID FUEL IN SINGLE PORT HYBRID ROCKET ...... 5168 J. Lee, S. Kim, G. Kim, H. Moon, J. Kim
NUMERICAL INVESTIGATION OF THE EFFECT OF A DIAPHRAGM ON THE PERFORMANCE OF A HYBRID ROCKET MOTOR...... 5178 N. Bellomo, M. Lazzarin, F. Barato, M. Grosse
NUMERICAL INVESTIGATION OF 2-D HYPERSONIC INLET STARTING CHARACTERISTIC CAUSED BY DYNAMIC ANGLE-OF-ATTACK...... 5194 K. Liu, K. Zhang
NUMERICAL SIMULATION OF THE AUTO-IGNITION OF ETHYLENE IN AN SCRAMJET COMBUSTOR WITH AIR THROTTLING...... 5203 J. Noh, J. Choi, J. Byun, J. Lim, V. Yang
INVESTIGATION ON 3-DIMENSIONAL EFFECT OF SHOCK WAVES CAUSED BY A STRUT-COWL SYSTEM IN A SCRAMJET ENGINE ...... 5217 S. Sato, T. Munakata, M. Ishikawa
AIRBREATHING ROTATING DETONATION WAVE ENGINE CYCLE ANALYSIS...... 5228 E. Braun, F. Lu, D. Wilson, J. Camberos
DETONATION ENGINE PERFORMANCE COMPARISON USING FIRST AND SECOND LAW ANALYSES ...... 5241 E. Braun, F. Lu, D. Wilson, J. Camberos
WAVE ROTOR COMBUSTOR AEROTHERMODYNAMIC DESIGN AND MODEL VALIDATION BASED ON INITIAL TESTING ...... 5255 T. Elharis, S. Wijeyakulasuriya, M. Nalim
MIXING AND IGNITION POTENTIAL OF TRANSIENT CONFINED TURBULENT JET IN A WAVE ROTOR COMBUSTOR ...... 5293 S. Wijeyakulasuriya, I. Perera, M. Nalim
EXPERIMENTAL INVESTIGATION ON THE WAVE ROTOR CONSTANT VOLUME COMBUSTOR ...... 5312 M. Yu, S. Meyer, M. Shimo, M. Kowalkowski, P. Snyder
CARMECA, 3-D BASIC TOOL FOR ENGINE ROCKET SIZING...... 5324 M. Ferlin, D. Tchou-Kien
HM7B SIMULATION WITH ESPSS TOOL ON ARIANE 5 ESC-A UPPER STAGE...... 5332 A. Isselhorst
COLD FLOW DILUENT MIXING STUDY USING RADIAL HIGH DENSITY RATIO JETS INTO A CIRCULAR FREESTREAM...... 5346 A. Le, I. Donovan, N. Sedano, R. Bernstein
MANUFACTURING AND TESTING OF TPX LH2-TURBOPUMP PROTOTYPE...... 5362 P. Fayolle, P. Fonteyn, F. Laithier, H. Olofsson, L. Forsberg, J. Dehouve, B. Pouffary, P. Supie
DESIGN OF A TEST SETUP FOR THE CHARACTERIZATION OF THE DYNAMIC TRANSFER MATRIX OF CAVITATING INDUCERS ...... 5374 A. Cervone, L. Torre, A. Pasini, E. Piccoli, L. D'Agostino
ROTORDYNAMIC FORCES ON A FOUR BLADED INDUCER ...... 5390 A. Pasini, L. Torre, A. Cervone, L. D'Agostino
CONVECTIVE AND RADIATIVE HEAT TRANSFER IN A THICK CYLINDER USING THE HEAT BALANCE INTEGRAL METHOD...... 5406 R. Driscoll
TEMPERATURE FIELD IN A CRYOGENIC LOX/CH4 SPRAY FLAME...... 5427 W. Clauss, C. Manfletti, J. Sender, M. Oschwald, V. Fabelinsky, V. Smirnov, O. Stel-Makh, K. Vereschagin
CATALYTIC COMBUSTION OF HYDROGEN-OXYGEN CRYOGENIC MIXTURES OVER CELLULAR CERAMIC-BASED CATALYSTS...... 5440 R. Amrousse, Y. Batonneau, C. Kappenstein, M. Theron, P. Bravais
AUTOIGNITION TESTS BY INJECTING KEROSENE INTO VORTEX OF DECOMPOSED HYDROGEN PEROXIDE ...... 5450 S. Jo, S. An, J. Kim, H. Yoon, S. Kwon
A DESIGN OF AN GIFFARD INJECTOR-PUMPED BIPROPELLANT MICRO-ROCKET...... 5459 N. Brikner, J. Protz
AN OVERVIEW OF THE DEVELOPMENT OF THE CATALYTIC IGNITER FOR THE NEXT GENERATION LAUNCHER...... 5470 B. Brauers, H. Snijders, W. Kwan, A. Mayer, R. Strunz, T. Kachler
A CONCEPTUAL SYSTEM DESIGN STUDY FOR A LINEAR AEROSPIKE ENGINE APPLIED TO A FUTURE SSTO VEHICLE...... 5485 T. Tomita, N. Kumada, A. Ogawara
EVALUATION OF CATALYTIC REACTORS FOR COMBUSTION STABILIZATION AT HIGH ALTITUDES...... 5493 J. Sisco, J. Hollman, J. Kerrebrock, B. Rock, S. Kearney, C. Lents
MODELING OF PLASMA REFORMING OF ETHANOL INTO HYDROGEN IN THE ELECTRIC DISCHARGE IN A GAS CHANNEL WITH LIQUID WALL ...... 5506 A. Shchedrin, D. Levko, V. Naumov, V. Chernyak, V. Yukhymenko, S. Olszewski
NEW TECHNOLOGY OF PLASMA REFORMING OF LIQUID HYDROCARBON FUELS IN DYNAMIC PLASMA-LIQUID SYSTEMS ...... 5516 V. Chernyak, S. Olszewski, V. Yukhymenko, S. Sidoruk, O. Nedgbaliuk, I. Prysiazhnevych, A. Shchedrin, D. Levko, V. Naumov, V. Demchina, V. Kudryavzev
EFFECT OF CHANNEL LENGTH ON MESO-SCALE SPIRAL COMBUSTOR PERFORMANCE ...... 5528 V. Vijayan, A. Gupta
SHOCK/BOUNDARY LAYER/HEAT RELEASE INTERACTION IN THE HYSHOT II SCRAMJET COMBUSTOR...... 5538 D. Cecere, A. Ingenito, L. Romagnosi, C. Bruno, E. Giacomazzi
LOOP SHAPING CONTROL DESIGN FOR A SUPERSONIC PROPULSION SYSTEM MODEL USING QFT SPECIFICATIONS AND BOUNDS ...... 5555 J. Connolly, G. Kopasakis
SIMULATION OF THE CONCORDANT CONTROL OF INLET/SERN OF THE HYPERSONIC AIRBREATHING VEHICLE UNDER OFF-DESIGN POINT...... 5574 R. Gu, J. Xu, J. Mo, K. Zhang
SENSITIVITY OF THE IGNITION-PERIOD SURFACE STRESS RESPONSE OF A COMPOSITE SRM NOZZLE TO IGNITION RATE...... 5585 J. Beaujardiere, E. Morozov, G. Bright
PRESSURE VARIATIONS IN ROCKET NOZZLES. PART 1: DIRECT ASYMPTOTIC PREDICTIONS...... 5601 B. Maicke, J. Majdalani
PRESSURE VARIATIONS IN ROCKET NOZZLES. PART 2: ANALYTICAL PREDICTIONS DURING BLOWDOWN...... 5612 B. Maicke, J. Majdalani, R. Geisler
PRESSURE VARIATIONS IN ROCKET NOZZLES. PART 3: DIRECT CALCULATION OF THE LOCAL MACH NUMBER...... 5624 J. Majdalani, B. Maicke
THERMOCHEMICAL EROSION ANALYSIS OF CARBON-CARBON NOZZLES IN SOLID-PROPELLANT ROCKET MOTORS...... 5631 D. Bianchi, F. Nasuti
NUMERICAL SIMULATION APPLIED TO NON-FUNCTIONAL STIMULI...... 5647 D. Idelot
VOLUME 7
ON THE COMPRESSIBLE HART-MCCLURE MEAN FLOW MOTION IN SIMULATED ROCKET MOTORS ...... 5657 B. Maicke, T. Saad, J. Majdalani
HYBRID PARTICLE SWARM–PATTERN SEARCH OPTIMIZER FOR AEROSPACE PROPULSION APPLICATIONS...... 5674 R. Jenkins, R. Hartfield
EXACT HAM SOLUTIONS FOR THE VISCOUS ROTATIONAL FLOWFIELD IN CHANNELS WITH REGRESSING AND INJECTING SIDEWALLS...... 5688 J. Majdalani, H. Xu, Z. Lin, S. Liao
QUASI-ANALYTICAL APPROXIMATION OF THE COMPRESSIBLE FLOW IN A PLANAR ROCKET CONFIGURATION ...... 5712 M. Akiki, J. Majdalani
A COMBUSTION INSTABILITY PHENOMENON ON A LOX/METHANE SUBSCALE COMBUSTOR ...... 5723 H. Kawashima, K. Kobayashi, T. Tomita, T. Kaneko
ARES-III: A SHUTTLE DERIVED HEAVY LIFT LAUNCH VEHICLE CONCEPT FOR EXPLORATION MISSIONS...... 5733 B. Donahue, L. Brady, M. Farkas, S. Leroy, N. Graham, D. Blue
VEGA SOLID ROCKET MOTORS DEVELOPMENT AND QUALIFICATION...... 5745 S. Bianchi, F. Serraglia, F. Giliberti, F. Betti, C. Milana
LOW SPOOL ELECTRICAL POWER EXTRACTION USING HARDWARE-IN-THE-LOOP METHODS ...... 5754 C. Miller, J. Zumberge, M. Corbett, M. Wolff, G. Russell
ENERGY MANAGEMENT OF AN AIRCRAFT ELECTRICAL SYSTEM ...... 5760 T. O'Connell, G. Russell, K. McCarthy, E. Lucus, J. Zumberge, M. Wolff
INVESTIGATING PREMATURE IGNITION OF THRUSTER PRESSURE CARTRIDGES BY MECHANICAL IMPACT OF INTERNAL COMPONENTS ...... 5772 S. Woods, R. Saulsberry
ION VELOCITY DISTRIBUTION IN A LOW-POWER CYLINDRICAL HALL THRUSTER...... 5779 N. Macdonald, M. Cappelli, W. Hargus Jr.
MAGNETIC FIELD EFFECTS ON THE PLUME OF A DIVERGING CUSPED-FIELD THRUSTER...... 5800 T. Matlock, S. Gildea, F. Hu, N. Becker, P. Lozano, M. Martinez-Sanchez
A PLASMA PROPULSION CONCEPTBASED ON DIRECT ION ACCELERATION WITH BEATING ELECTROSTATIC WAVES...... 5810 B. Jorns, E. Choueiri
MICRO-MULTI-PLASMAJET ARRAY THRUSTER ...... 5829 H. Horisawa, S. Hagiwara, I. Funaki
RE-GENERABLE FIELD EMISSION CATHODES PART II: QUENCHED EMITTER PERFORMANCE ANALYSES...... 5837 J. Makela, R. Washeleski, L. King
SPATIALLY-RESOLVED STUDY OF INTER-CUSP TRANSPORT AND CONTAINMENT OF PRIMARY ELECTRONS...... 5851 A. Hubble, J. Foster
IN-FLIGHT OPERATION OF THE DAWN ION PROPULSION SYSTEM: STATUS AT ONE YEAR FROM THE VESTA RENDEZVOUS ...... 5863 C. Garner, M. Rayman
STATUS OF THE NASA’S EVOLUTIONARY XENON THRUSTER (NEXT) LONG-DURATION TEST AFTER 30,352 HOURS OF OPERATION ...... 5882 D. Herman
DESIGN OF A DUAL STAGE GRIDDED ION ENGINE FOR THE HIPER PROJECT...... 5914 M. Coletti, S. Gabriel
PERFORMANCE EVALUATION OF THE T6 ION ENGINE...... 5926 J. Snyder, D. Goebel, R. Hofer, J. Polk, N. Wallace, H. Simpson
SIMULATION OF COUPLED SUPERSONIC INLET AND A FAN...... 5939 D. Voytovych, C. Merkle
A COMPARISON OF DIFFERENT GAS TURBINE ENGINES GROUND VORTEX FLOWS...... 5950 J. Barata, P. Manquinho, A. Silva
DEVELOPMENT OF REGRESSION FORMULAS FOR CAMUI TYPE HYBRID ROCKETS AS FUNCTIONS OF LOCAL O/F...... 5961 H. Nagata, S. Hagiwara, Y. Kaneko, M. Wakita, T. Totani, T. Uematsu
INTRODUCTION TO THE UNIVERSITY OF KWAZULU-NATAL HYBRID SOUNDING ROCKET PROGRAM ...... 5975 M. Brooks, J. Beaujardiere, S. Chowdhury, B. Genevieve, L. Roberts
EXPERIMENTAL INVESTIGATIONS OF TAPERED FUEL REGRESSION RATE OF HYBRID ROCKET MOTOR...... 5983 J. Kim, S. Kim, J. Kim, H. Moon
VARIABLE THRUST, MULTIPLE START HYBRID MOTOR SOLUTIONS FOR MISSILE AND SPACE APPLICATIONS...... 5995 B. Austin Jr., S. Heister, E. Dambach, S. Meyer, E. Wernimont
EXPERIMENTAL INVESTIGATION OF SUPERSONIC COMBUSTION IN THE HIEST AND HEG FREE PISTON SHOCK TUNNELS...... 6009 J. Schramm, T. Sunami, K. Ito, K. Hannemann
SCRAMJET ENGINE COMBUSTOR TESTS IN A SUPERSONIC WIND TUNNEL WITH A VITIATED AIR HEATER ...... 6027 S. Kang, Y. Lee, S. Yang, B. Choil
DEVELOPMENT OF A LAB-SCALE GEL FUEL RAMJET COMBUSTOR ...... 6038 A. Kuznetsov, Y. Solomon, B. Natan
INCORPORATION OF A TRADE STUDY TOOL FOR FUELS DEVELOPMENT WITHIN SRHEATTM ...... 6050 N. Pearson, D. Giel, J. Gutierrez
REGENERATIVE COOLING EFFICIENCY OF SEVERAL SYNTHETIC AND JET FUELS AND PRELIMINARY COMBUSTION-PYROLYSIS COUPLING...... 6066 N. Gascoion, G. Abraham, P. Gillard
DEVELOPMENT AND TESTING OF A HIGH TEMPERATURE N2O DECOMPOSITION CATALYST ...... 6087 D. Wickham, B. Hitch, B. Logsdon
DESIGN OF A CATALYTIC NITROUS OXIDE DECOMPOSITION REACTOR ...... 6101 B. Hitch, D. Wickham
UNIFIED LOW-RISK SINGLE-SHAFT TURBOPUMP FOR CRYOGENIC EXPANDER-CYCLE ROCKET ENGINES ...... 6111 S. Bouley, R. Grabowksi Jr., V. Rachuk, A. Dmitrenko, A. Ivanov
PISTONLESS PUMP SYSTEM FOR ACCELERATED DEVELOPMENT OF A HEAVY LIFT LOX HYDROCARBON ENGINE...... 6125 S. Harrington
OPTICAL MASS GAUGING SYSTEM FOR MEASURING LIQUID LEVELS IN A REDUCED GRAVITY ENVIRONMENT ...... 6135 R. Sullenberger, W. Munoz, M. Lyon, K. Vogel, A. Yalin, V. Korman, K. Polzin
DEVELOPMENT AND CHARACTERIZATION OF A PARTICLE-IMPACT IGNITION FACILITY...... 6144 M. Crofton, P. Stout, T. Albright, M. Worshum, J. Emdee, E. Petersen
PARTICLE IMPACT IGNITION IN HIGH PRESSURE OXYGEN: INITIAL RESULTS...... 6165 M. Crofton, E. Petersen
MODELING OF LOX/METHANE IMPINGEMENT, MIXING AND COMBUSTION ...... 6177 N. Harpal, E. Besnard, R. Toossi
COUPLED LEVEL-SET/VOLUME-OF-FLUID METHOD FOR THE SIMULATION OF LIQUID ATOMIZATION IN PROPULSION DEVICE INJECTORS ...... 6188 M. Arienti, X. Li, M. Soteriou, C. Eckett, R. Jensen
ON THE NONLINEAR DYNAMIC RESPONSE OF ROCKET SWIRL\R\NINJECTORS...... 6198 M. Ismailov, S. Heister
SIMULATION OF INJECTION OF SHEAR-THINNING GEL PROPELLANTS THROUGH PLAIN-ORIFICE ATOMIZER...... 6225 C. Yoon, S. Heister, G. Xia, C. Merkle
EFFECT OF INJECTOR WALL HEAT FLUX ON CRYOGENIC INJECTION ...... 6243 D. Banuti, K. Hannemann
RHEOLOGICAL CHARACTERIZATION OF HYDROXYPROPYLCELLULOSE/MONOMETHYLHYDRAZINE AND\R\NSILICA/RED FUMING NITRIC ACID GELS ...... 6252 T. Kubal, R. Arnold, T. Pourpoint, O. Campanella, W. Anderson
DYNAMICS OF SHEETS FORMED USING GELLED PROPELLANT IMPINGING JETS...... 6269 J. Mallory, P. Sojka
FORMULATION OF GELLED PROPELLANT SIMULANTS ...... 6277 J. Mallory, S. Defini, P. Sojka
HYPERGOLIC IGNITION OF OXIDIZERS AND FUELS BY FUEL GELATION AND SUSPENSION OF REACTIVE OR CATALYST PARTICLES...... 6286 B. Natan, V. Perteghella, Y. Solomon
HIGH SPEED VISUALIZATION OF LOX/GH2 ROCKET INJECTOR FLOWFIELD: HOT-FIRE AND COLD- FLOW EXPERIMENTS ...... 6293 J. Locke, S. Pal, R. Woodward, R. Santoro
MEASURING TRANSVERSE STABILITY COMBUSTION RESPONSE AT FULL SCALE FREQUENCIES IN A SUBSCALE COMBUSTOR...... 6311 B. Pomeroy, N. Nugent, W. Anderson
EVALUATION OF SPARK PLASMA SINTERING (SPS) FORMING METHOD FOR LIQUID ROCKET COMBUSTION CHAMBERS ...... 6322 T. Masuoka, S. Moriya, A. Kurosu, A. Kumakawa
DEVELOPMENT OF A COMBUSTION STABILITY ANALYSIS TOOL INCORPORATING DETAILED FLAME-VORTEX DYNAMICS...... 6329 J. Sisco, S. Shanbhogue, H. Asrag, A. Ghoniem
PREDICTION OF THERMOACOUSTIC LIMIT CYCLES DURING PREMIXED COMBUSTION USING THE MODIFIED GALERKIN APPROACH ...... 6339 H. Krediet, W. Krebs, J. Portillo, J. Kok
CELLULAR INSTABILITIES FROM THE ONSET OF CELLS UNTIL EXTINCTION IN A NON-PREMIXED OPPOSED-FLOW TUBULAR FLAME ...... 6357 S. Shopoff, R. Pitz, P. Wang
ANALYSIS OF FLOW-FLAME INTERACTIONS IN A GAS TURBINE MODEL COMBUSTOR UNDER THERMO-ACOUSTICALLY STABLE AND UNSTABLE CONDITIONS...... 6376 A. Steinberg, I. Boxx, M. Stohr, W. Meier, C. Carter
EFFECTS OF UNSTEADY HEAT RELEASE ON LIQUID ROCKET COMBUSTION INSTABILITY ...... 6398 T. Rice, G. Flandro, P. Gloyer
EFFECTS OF NANOALUMINUM ON DROPLET COMBUSTION AND COMBUSTION INSTABILITIES IN A SINGLE ELEMENT ROCKET COMBUSTOR...... 6412 M. Pfeil, S. Rosen, Y. Yu, W. Anderson, S. Son
EVALUATION OF COMBUSTION PERFORMANCE OF ALTERNATIVE AVIATION FUELS ...... 6421 T. Edwards, C. Moses, F. Dryer
VELOCITY COUPLING FROM PULSE TEST FIRINGS...... 6442 C. Rousseau, J. Knoetze
BOUNDARY LAYER TREATMENT OF THE POROUS CHANNEL FLOW WITH WALL REGRESSION...... 6458 J. Majdalani, C. Zhou
EFFECTS OF TEMPERATURE CONDITIONED ENVIRONMENT ON A PROPELLANT’S PRESSURE- COUPLED RESPONSE ...... 6469 J. Spurling, F. Blomshield, D. Pate
LARGE EDDY SIMULATION FOR LOW FREQUENCY OSCILLATIONS IN TAIL-PIPE NOZZLE SOLID ROCKET MOTORS...... 6478 Q. Zhang, J. Li, W. Wang, N. Wang
INTERNAL BALLISTICS SIMULATION OF NAWC TACTICAL MOTORS WITH SPINBALL MODEL...... 6490 E. Cavallini, B. Favini, M. Giacinto, F. Serraglia
THE INTERNAL FLOW MODELING OF A SIMULATED SOLID PROPELLANT-LINER DEBOND USING LOCI-CHEM ...... 6518 C. Hood, J. Sims, N. Knight
CORRELATION OF MIDWEB ANOMALY WITH MICROSTRUCTURE OF COMPOSITE PROPELLANT ...... 6525 K. Kitagawa, T. Shimada, H. Hasegawa, M. Fukunaga, H. Miyachi
THE IMPACT OF WALL ANGLE ON NOZZLE SEPARATION BEHAVIOR...... 6532 A. Aghababaie, N. Taylor
SYSTEM DESIGN OF A REUSABLE, HORIZONTAL TAKE-OFF/HORIZONTAL LANDING TWO STAGE TO ORBIT VEHICLE...... 6545 P. Griesemer, J. Mueller, J. Du, M. Paluszek
EVALUATION OF CFD CODES FOR HYPERSONIC FLOW MODELING ...... 6569 B. Maicke, J. Majdalani
Author Index