16th JANNAF Combustion Meeting, Naval Postgraduate School, Monterey, California, September 10-14, 1979: Nitramine and solid rocket propellants, ramjets, and liquid bipropellants (unclassified

Chemical Propulsion Information Agency, 1979 - Ordnance

Contents

• BURN RATE BEHAVIOR OF HIGH DENSITY BINDERLESS HMX 1: 3
• NITRAMINE DECOMPOSITION: 17
• KINETICS OF NITRAMINE FLAME REACTIONS: 35
• ELECTRON SPIN RESONANCE STUDIES OF HMX AND RDX THERMAL DECOMPOSITION: 51
• THERMAL DECOMPOSITION OF HMX: 59
• NAVY LOVA PROPELLANT DEVELOPMENT: 73
• NOROLL PROCESS OF PRODUCING NITRAMINE GUN PROPELLANTS: 83
• EFFECTS OF PRESSURE AND MELTING BEHAVIOR ON THE COMBUSTION: 95
• A PRIORI THERMOCHEMISTRY AND RATE CONSTANT ESTIMATES FOR FLAME: 113
• COMBUSTION OF NONALUMINIZED BINDERS IN TAPERED SANDWICHES: 127
• EFFECT OF EROSIVE BURNING ON PRESSURE AND TEMPERATURE: 153
• AN INVESTIGATION OF THE EFFECTS OF FORMULATION PARAMETERS ON EROSIVE: 171
• ANALYSIS OF AMMONIUM PERCHLORATE COMBUSTION IN A TURBULENT FLOW: 193
• EFFECT OF BINDER TYPE ON ALUMINUM COMBUSTION AND ALUMINUM: 225
• APPLICATION OF ADVANCED OPTICAL SPECTROSCOPIC METHODS: 237
• TEMPORAL AND SPATIAL LOCATION OF THE TRANSITIONTODETONATION: 245
• TESTING OF A UNIQUE IGNITION SYSTEM FOR LARGE SOLIDPROPELLANT: 257
• THEORETICAL DETERMINATION OF NOZZLE ADMITTANCES USING A FINITE: 273
• ASSESSMENT OF CHAMBER PRESSURE OSCILLATIONS IN THE SHUTTLE SRB: 287
• PRELIMINARY EXPERIMENTS ON ACOUSTIC OSCILLATIONS DRIVEN: 305
• ON RESPONSE FUNCTIONS FOR COMPOSITE SOLID PROPELLANT: 321
• DIRECT MEASUREMENTS OF ACOUSTIC ADMITTANCE USING LASER DOPPLER: 343
• ROTATING VALVE FOR VELOCITY COMBUSTION RESPONSE MEASUREMENTS: 363
• INVESTIGATION OF THREE VELOCITY COUPLED TBURNER DESIGNS: 385
• STUDIES OF MOTOR INSTABILITY PROBLEMS: 399
• A PRIMITIVE VARIABLE COMPUTER MODEL FOR COMBUSTION WITHIN: 429
• LINSTABILITY IN DUCTED ROCKET FUEL GENERATORS: 451
• DEVELOPMENT OF A PHOTON CORRELATION LASER VELOCIMETER FOR: 461
• EVALUATION OF CARS IN A PRACTICAL COMBUSTION ENVIRONMENT: 471
• INVESTIGATION OF THE FEASIBILITY OF CARS MEASUREMENTS IN SCRAMJET: 487
• COMPARISON OF THERMOCOUPLE GAS SAMPLING AND RAMAN MEASURED: 511
• FLOWFIELD STUDIES OF DUMP COMBUSTORS: 529
• MEAN DROPLET DIAMETER RESULTING FROM ATOMIZATION OF A TRANSVERSE: 541
• REDUCTION OF COMBUSTION EFFICIENCY ASSOCIATED WITH LIQUID PHASE: 557
• HIGH DENSITY FUELS: 569
• EFFECT OF GRAZING FLOW ON THE NONLINEAR ACOUSTIC BEHAVIOR: 579
• ADMITTANCES AND CHARACTERISTIC COMBUSTION TIMES OF REACTIVE GASEOUS: 605
• DESIGN AND EVALUATION OF HIGH PERFORMANCE ROCKET ENGINE INJECTORS: 617
• INVESTIGATION OF A PUTTY PROPELLANT TURBINE POWER SYSTEM: 645
• A MECHANISM FOR THE PHOTOCHEMICAL INDUCED COMBUSTION OF H2F2: 657
• SUBJECT INDEX: 669
• SOURCE INDEX: 677
• DISTRIBUTION LIST: 685

Bibliographic information

• Title: 16th JANNAF Combustion Meeting, Naval Postgraduate School, Monterey, California, September 10-14, 1979: Nitramine and solid rocket propellants, ramjets, and liquid bipropellants (unclassified; Volume 2 of 16th JANNAF Combustion Meeting, Naval Postgraduate School, Monterey, California, September 10-14, 1979, Joint Army-Navy-NASA-Air Force Interagency Propulsion Committee. Combustion Subcommittee; Volume 308 of CPIA publication
• Contributors: Joint Army-Navy-NASA-Air Force Interagency Propulsion Committee. Combustion Subcommittee, Chemical Propulsion Information Agency
• Publisher: Chemical Propulsion Information Agency, 1979