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HEMCE 2011- List of Accepted Papers for Poster Presentation

S.No. Title Approximate Method for Determining Electrically Driven Flyer Velocity By Dent on Metal Plate Induced Acoustic Investigation of Laser Sock Waves and Viberation from Solids Instrumentation Technique for Static Testing of Large Scale Rocket Motor Development Of Electronic Delay Detonator Towards understanding micro-blast waves from a polymer tube coated with milligram range for Measurement Electrical Techniques HMX charge of Detonics Parameters Of High Explosives ammunition for shock on Dual HESH shock interaction to achieve enhanced behind the armour effect Development of Detonation Logic based Multipoint Initiation System for High Explosives Indigenous Development &Fabrication of Shock Sensors for Detonics & Shockwave Research Strategies for Identification of High Energy Materials using Laser Induced Breakdown Spectroscopy using Strategies for Identification of High Energy Materials using Laser Induced Breakdown Spectroscopy ­Ratiometric LIBS Studies on Nitromethane and Simple Liquid Fuels using Nanosecond PulsesDetection and Analysis of Rapid Improvised Explosive Compositions Made up of Hydrogen Nano Tubes Functionalized Carbon Peroxide and (CNT): An Innovative Way to Electrochemical Sensing Of Explosives Explosives Detection: Exploitation of the Chemical and Physical Signatures Conceptual Design of Rocket Launched Decoy for Under water Applications Design Optimization of Gas Generator for Ignition of fuel in Thermal Engine Design Of A Booster With Hmx/Vitona (95:05) EFFECTS OF CROWBAR SHAPE AND LOCATION ON THE PERFORMANCE OF AN EXPLOSIVE Voltage Pulse Power Compact High DRIVEN HELICAL FLUX Source for EBW initiation Principal Author DR.DINESH KUMAR PAL Ch.Leela Sandeep Kumar A.Sudheer Babu Obed Samuelraj I P.C. Gautam V. Anguswamy Rajneesh Gupta Anil Kumar G. MANOJ KUMAR G. MANOJ KUMAR S. Sreedhar S.S.Mhase Affialation Category

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20

TBRL, Chandigarh ACRHEM, Hyderabad HEMRL, Pune HEMRL, Pune IISc Bangalore TBRL, Chandigarh PXE, Chandipur TBRL, Chandigarh TBRL, Chandigarh ACRHEM, Hyderabad ACRHEM, Hyderabad ACRHEM, Hyderabad HEMRL, Pune

DET DET DET DET DET DET DET DET DET DT DT DT DT DT DT EMA EMA EMA EMA EMA

Shikha Kapila/Sakshi Arora TBRL, Northwest PacificChandigarh National Dr. David A. Atkinson Laboratory A. Srinivas Kumar K.U.Gokul Partha Sarkar Vijay Kumar Yogeshwar Nath NSTL, Vizag NSTL, Vizag TBRL, Chandigarh TBRL, Chandigarh TBRL, Chandigarh

21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41

A study on chemical additive based methods for prevention of agglomeration of Ammonium Studies on Development of Modular Charge System for 105 mm IFG Studies on Titanium Based High Temperature and Suffocating Smoke Producing Composition Development of High Explosive Based Rotor Blade Ejection Technique for Turbojet Aircraft Engine Testing Studies of Al/KClo4 hermite composistion for closed system application Of A Nozzle Closure For Development S200 Strap On Booster Development Of Reverse Flow Multiple Nozzle Solid Rocket Motor Study on the Enhancement of Regression Rate of Hybrid Rocket using Swirl Flow for Paraffin wax SMOKE CLASSIFICATION OF REDUCED NITRAMINE BASED COMPOSITE PROPELLANT Nano-fluid based on MMH/NanoAluminium for Improved Regenerative Cooling in Liquid Rocket Engines of A Study on Probable Failure Modes 1A/1W Detonator Design of Through Bulkhead Initiator Thermal ignition of High Energy materials by pulse lasers Experimental Investigations of Hydrocarbon Fueled Scramjet Combustor by Employing High on the Role of Nature of Discreteness Burn-rates of Heterogeneous Energetic Materials Random Model for the 3D Discrete Combustion of the Heterogeneous Energetic of structural and Influence Materials physicochemical properties of molecules on the impact for FOX-7 of Reactive flow simulation sensitivity process Theoretical Evaluation of Gun Propellant for Dynamic Firing Computational Studies on Nheterocycle Functionalized Polyethers for High Energy Material Applications Heat Transfer Analysis Of Solid Rocket Motor During Curing Process

S Das RR Sanghavi A G Nagarkar M.Nallaperumal S K SAHU Shri PM Anthonies Shri K Sreejith Rajiv Kumar Jayesh Upadhyay Sreejith M Rani Krishnan K.R

HEMRL, Nasik HEMRL, Pune HEMRL, VSSC, Pune Thiruvananthapur am HEMRL, VSSC, Pune Thiruvananthapur am VSSC, Thiruvananthapur am IIT Chennai HEMRL, VSSC, Pune Thiruvananthapur am VSSC, Thiruvananthapur am VSSC,

EMA EMA EMA EMA EMA EMA EMA EMA EMA EMA EMA EMA EMA EMA M&S M&S M&S M&S M&S M&S M&S

Thiruvananthapur Ranjith Kumar Reddy G am Manpreet Singh C. Chandrasekhar G. MANOJ KUMAR G. MANOJ KUMAR Vladimir K. Golubev P M Jadhav T.K.Chakraborthy S.Radhakrishnan Bejoy T TBRL, Chandigarh DRDL Hyderabad ACRHEM, Hyderabad ACRHEM, Hyderabad Russian Federal Nuclear Center ­ VNIIEF, Sarov HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune

42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62

ANALYSIS ON GRAIN STRUCTURAL INTEGRITY OF GUN LAUNCHED ROCKET ASSISTED PROJECTILE- RANGE A correlation study between impact sensitivity and bond electron density of energetic molecules A MODEL FOR ESTIMATING PROPELLANT GRAIN CURING SCHEDULE study of predictive Comparative models for gas explosions Reactive Flow Modelling of Transient Detonation Waves Start-up Transient Simulation in Solid Rocket Motors Structural analysis of the Frangible ring in low shock XTA based separation systems Computation of Vibrational Frequencies and Structures for energetic molecules and their products Crystal density of high energetic molecules from ab initio crystal structures: Some challenges Computational study of structural, elastic constants and related mechanical properties and their on Temperature and density effects liquid nitromethane: A molecular dynamics study Cure kinetic modeling of thermosetting composite-polymeric system Theoretical Charge density studies on some Amine azide propellant molecules Investigations on Tetrazole Theoretical Derivatives Modeling of Hypervelocity Projectile Acceleration in a Fast Shock Tube Launcher Nozzle Machining of Ballistic Evaluation Motor Post Curing Operational Issues in Large Size Solid Propellant Rocket Motor Processing Ultraviolet Spectroscopy-A Quality Control Tool for Estimation of Purity of Liquid Gun Propellant Compositions Study of SAG Behaviour on Agni Class of Solid Rocket Motor Use of Visible Spectral Region in Determination of Age of Solid Propellants Drying of Low Melting point & highly Hygroscopic Crystalline solid ingredients of Composite Propellant

P. Sunitha A.K. Sikder

RCI Hyderabad HEMRL, Pune

M&S M&S M&S M&S M&S M&S M&S M&S M&S M&S M&S M&S M&S M&S M&S MQI MQI MQI MQI MQI MQI

P.V.N.L. Syamala Devi ASL, Hyderabad Dipti.B Aaditya V. Majalee K Khadar Voli Shitij Arora Poonam Pahari P.Kumaradhas K. Ramesh Babu S. Appalakondaiah Ravishankar PM M. Nagarajan Shaibal Banerjee Vishal Mehra K.KISHORE KUMAR K.KISHORE KUMAR R.R. MAHAJAN B. MAHESH P.H. Kulkarni CFEES Delhi BARC, Visakhapatnam VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am BARC, Visakhapatnam Periyar University, Salem /HEMRL ACRHEM, Hyderabad ACRHEM, Hyderabad SHAR, ISRO, Sriharikota Periyar University, Salem /HEMRL DIAT, Pune BARC, Visakhapatnam SF Complex, DRDO, Jagdalpur SF Complex, DRDO, Jagdalpur HEMRL, Pune SF Complex, DRDO, Jagdalpur CQA (ME ), Kirkee

SF Complex, PURUSHOTTAM SINGH DRDO, Jagdalpur

63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83

Development of Collapsible Mandrel for Solid Propellant Casting Scope of Rework in Composite Rocket Motor Case AFTER INSULATION LINING Interchangeability of Segments in Rocket Motor Processing Parameter Optimization for CNC Milling of High Explosives Development of Single Base Propellant for Large Calibre Gun Studies on Effect of Process Parameters on Ballistics of Single Base Gun Propellants Studies on web size variation of Double Base Gun Propellants on CV Results Surface Coating of Single Base Propellant for High Calibre Guns DESIGN OPTIMIZATION OF HOT AIR CURING OVENS USED FOR CURING OF LARGE DIAMETER Mechanism for Fork Type Locking SOLID ROCKET Autoclave Flanged Door Study on scalability of composite propellant compositions from subscale to production levels in vertical Development of an Alternative Method for the Purity Determination of Boron by Flame Atomic Absorption Quantification of Tris-1-(2 Methyl Aziridinyl) Phosphine Oxide (MAPO) by Gas Chromatography for Conventional Method Quantification of Polyvinyl Acetate (PVAc) and Cellulose in Resin Based Development of a new method for the determination of ammonium perchlorate content in process to Development of a new propellant improve the storage life of Ultra fine Ammonium Perchlorate(UFAP) assisted Novel and efficient microwave synthesis of 3-Amino-5-nitro-l, 2, 4triazole of Gunayl insensitive high Analysis(ANTA): anUrea Dinitramide (GUDN) and its Precursor Using Ion Chromatography and HPLC Analysis of 2,4-dinitroanisole by using Reverse Phase High Performance Liquid Chromatography (RP-HPLC) Production oriented sleeve inhibition technique for small scale Extruded Double on effect of variables Studies Base (EDB) propellanton interface properties in case bonded solid rocket propellant motors

K.KISHORE KUMAR U.Suresh Babu Deo Kumar Verma Rajeev Kumar Vruushali Khire Vruushali Khire C. N. Divekar Vasudha Kaul B.Sanyal Manoj Kumar B Bhattacharya Abhay Yadav A P Singh S.S.Mhase Mehilal S Nandagopal D M Badgujar D M Badgujar A.K. Sikder KG Bhalerao SB Navale

SF Complex, DRDO, Jagdalpur SF Complex, DRDO, Jagdalpur SF Complex, DRDO, Jagdalpur TBRL, Chandigarh HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune SF Complex, DRDO, Jagdalpur HEMRL, Nasik HEMRL, Nasik HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune

MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI

84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99

Repair of insulation and study of interface bonding property DSC study of the cure kinetics on Poly Nitratomethyl Oxetane (PLN) with different isocyanates Prediction of end of mix viscosity of composite propellant slurry by wetting constant Studies on Effect of Different Web Sizes of Single Base Gun Propellants on Closed on Application of StudiesVessel (CV) resultsSegmented Mandrel in Case Bonded Large Size Rocket Motor Extrusion Technique for ECP grain Induction of 8 liters capacity vertical mixer for propellant qualification trials ­ optimization of process parameters Burning rate and particle size distribution of Ammonium Perchlorate (AP) based propellant -Experience with Feasibility studies on D-T Based Sealed Tube Neutron Generators for Neutron Radiography Applications Neutron radiography OF SPACE Ordnance System STUDIES ON DRYING CHARACTERISTICS OF AMMONIUM PERCHLORATE Digital Radiography of Large Size Solid Rocket Motors with High Energy X-Ray from LINAC using Computer Computer Radiography (CR) for Inspection of Propellant Grains using 450 Film X-Ray Radiographic DualkV X-Ray Source Technique for Non-Destructive Evaluation (NDE) of Propellant Grains Ultrasonic Testing as a Complementary NDE method for Inspection of EDB Propellant Grains COMBUSTION INSTABILITY IN SOLID ROCKET MOTORS

SB Navale Kavita Ghosh K Ramesh Vruushali Khire Mukesh Jain Ajay N Patil Isaac Sam Senthil Kumar Cherian Thomas R Gunasekaran Ramachandra Rao A Bikash Ghose Bikash Ghose V P Mall S S Pundale Mukane S.B Ghume S.G

HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, VSSC, Pune Thiruvananthapur am VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune

MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI MQI PT PT

INTERNAL BALLISTICS PREDICTION OF 100 SOLID ROCKET MOTORS THROUGH INCREMENTAL ANALYSIS Explosive Quality Control of Linear 101 Cords A Study on the Deformation Behaviour 102 of the Insulation Loose Flap in Booster Motor during of an Analytical Method Development Propellant Casting 103 for Analysis of IR and Visual Flare Compositions Effect Of Cellulosic Binders On Barium 104 Ferrocyanide ­ Potassium Perchlorate Based Igniter Composition

ARDE, Pune VSSC, Thiruvananthapur Biswa Ranjan Mohanty VSSC, am Aditya Bhattacharya Abhay Yadav S H Kulkarni Thiruvananthapur am HEMRL, Pune HEMRL, Pune

Effect of Barium Stearate on MTV 105 based Infra Red (IR) Flare Performance Development of pyrotechnic 106 composition for multispectral target Effect of HTPB on sensitivity of 107 pyrotechnic composistions based on Zirconium/Titanium/Nickel Effect of particle size of silicon and 108 potassium perclorate and additional oxidisers on burning rates based Studies on effective anti thermal anti 109 laser smoke screen on enhanced duraton Development and Qualification testing 110 of Cartridge Signal Flare Evaluation of a Reactive Material for 111 Controlled ignition of explosives Natural Frequency Criteria for Design 112 of Static Test Bed A Case Study on Burn Rate 113 Dependency on High Operating Pressure for a of Deterred 6/7 Ballistic study High Burn Rate 114 Propellant Used in Medium Caliber Ammunition Sensitivity Study Of Temperature 115 Multitubular Geometry Lova Gun Propellant Development Of Blank Ammunition 116 For Mbt Tank Charge Design Evaluations for Modular 117 Artillery Charge System for 130 mm FG Effect of Poisson's ratio on structural 118 integrity evaluation of solid propellant rocket on Sensitivity Studiesmotor grains Characteristics of 119 Advanced High Energy Solid Rocket Propellant Study On Combustion Instability Of 120 Solid Rocket Propellants By T-Burner An Ftir Method For The Prediction Of 121 Modulus Values Of Propellant Design of Improvised EBW Detonator 122 to Initiate TATB based Explosives through Numerical the sensitivity and Effect of binder on Simulation 123 thermal behaviour of magnesium/potassium MODIFIERS ON EFFECT OF BURN RATE notrate 124 A HYBRID BINDER SYSTEM BASED EXTRUDED COMPOSITE PROPELLANT Design, Development and Validation of 125 composite slabs against Dynamic blast load.

S. Debnath M N Manda Sabera Shaikh S L Deshpande P P Singh AK Sahu

HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune ARDE, Pune

PT PT PT PT PT PT PTE PTE PTE PTE PTE PTE PTE PTE PTE PTE PTE PTE PTE PTE PTE

Nausheen Al-Shehab US Army ARDEC R R Shukla PK Adak S M Dahiwale M.A.R.Shaikh M.A.R.Shaikh Vruushali Khire Bipin Kumar Bihari D Bhowmik Sunil Jain Sangeeta Sivanath Bhupinder Sewak Kulkarni MP K S Mulage Rajesh Mishra HEMRL, Nasik HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune VSSC, Thiruvananthapur am TBRL, Chandigarh HEMRL, Pune HEMRL, Pune CFEES Delhi

Studies on the Ignition Characteristics 126 of Low Burning Rate Composite Propellants using CO2 Laser Ignition Investigation of RF Emissions from 127 Laser produced plasma in air Fault Tree Analysis of Failure of GES 128 model in Life Assessment Trials Automated hardware-program system 129 to determine parameters of air-shock waves of Impact Tests to Study the Fragmenthigh-energy compositions 130 Detonation Characteristics of ScaledDown PJ-10 Warhead Trial Methodology for Fragment 131 Velocity Measurement to Evaluate PerformanceCharacterization and Preparation, of Warheads 132 Thermolysis of Transition Metal perchlorates with perchlorate and 2, 2`Coupling Reactions: An Efficient 133 Synthetic Strategy to 1,2,4-triazole Containing Polynitrobenzene Hot "Spectrothermoanalytical and

P.Sridharan L. Vinoth Kumar SS Khandagale S.Yu. Kulev Rajeev Kumar Pankaj Soni DINESH KUMAR AKHILA K.SAHOO

VSSC, Thiruvananthapur am ACRHEM, Hyderabad ARDE, Pune JSC FR & PC ALTAI, Biysk TBRL, Chandigarh TBRL, Chandigarh Gorakhpur University, Gorakhpur ACRHEM, Hyderabad HEMRL, North Pune Maharashtra University, Jalgaon Russian Federal Nuclear Center ­ VNIIEF, Sarov TBRL, Chandigarh TBRL, Chandigarh TBRL, Chandigarh HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune

PTE PTE PTE PTE PTE PTE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE

R.R. MAHAJAN 134 Stage Microscopical Investigations of some High Energy Materials" Synthesis of Energetic Tetrazoles Using Mukesh B. Deshmukh 135 ß-Cyclodextrin as A Superamolecular Catalyst charged and excited states on Effect of 136 the decomposition mechanisms of triaminotrinitrobenzene and Study Of Solidification Behaviour In 137 Melt Cast Tnt Based Compositions Small CaliberOf Tatb/Vitona Charges Compaction Spherical And 138 Isostatically Achieving Different Densities And To and numerical study An experimental Study The Detonator 139 to analyze the impact sensitivity of high explosives transfer in a batch Analysis of heat 140 reactor for nitration of 2-methyl-4,6pyrimidinedione Process Optimization for Preparation 141 of 1, 2, 4-triazol-5-one (Triazolone) Studies on preparation of 1,1-Diamino142 2,2-dinitroethene (FOX-7) particle with multimodal distribution Non-aqueous precipitation technology 143 for fine -HMX preparation Method for preparation and 144 characterization of 5-amino-, 5guanylamino-tetrazolium nitrate Synthesis of 1-Methyl-2,4,5145 trinitroimidazole (MTNI) from 1Methylimidazole: A melt-cast ­ Studies On Azidopropylesters 146 Energetic Plasticizers Vladimir K. Golubev Partha Sarkar Dhirendra Gupta Rajeev Kumar A.K. Mandal A.K. Mandal A.K. Mandal R P Diwakar A.K. Sikder A.K. Sikder MS Malwade

Ultra-sonication study and its Effect on 147 particle size and shape of BDNPN Thermal Decomposition Studies on 4, 148 10-Dinitro-2, 6, 8, 12- tetraoxa-4, 10diaza-tetracylododecane (TEX) using PyPyrolysis GCMS to Study 149 Decomposition Mechanism of PE-PCP Binder Application of Gas Chromatography150 Mass Spectrometry for Identification of Elemental Sulfur inon DNAN&TNT Comparative Studies Explosives 151 based Melt Cast HE formulation Feasibility studies on TATB based melt 152 cast explosive formulation A New Thermally stable and Insensitive 153 High Explosive: 2, 6-diamino-3, 5dinitropyrazine-1-oxide (LLM-105) of Studies on Tailoring of Particle size 154 Spheroidal NTO Particle size reduction of HMX by 155 ultrasonication and atisolvent recrystallizaton Theoretical analysis of inherent 156 instability of nitro explosives using homodesmic reactions and molecular Performance Evaluation Studies of 157 Cellulose Acetate Butyrate (CAB) based High Energy Materials Safety Evaluation of Polyol Pre 158 Polymer based High Explosive Compositions used in Spacereduce the Mechanistic approaches to 159 sensitivity of energetic organic compounds for insensitive munition Synthesis and Characterization of 160 Novel Energetic Poly Azido Esters Nano Structured Continuous Thin Film 161 of Energetic Material by Spin Coating Method Crystal structure prediction and the 162 Charge density distribution of High energeticIONIC LIQUIDS AS NEW ROLE OF Dimethyl nitraminotetrazole 163 ENERGETIC MATERIALS IN THE DEVELOPMENT OFImplementation of Development and ADVANCED 164 TDI Weighment & Transfer System For Solid Propellant Processing Iridium supported catalysts for 165 decomposition of hydroxylammonium nitrate on Application of Maxwell Studies 166 Fluid Model to Tensile Testing Curves of Different Classes Temperature on Studies on Effect of of Solid Rocket 167 Mechanical Properties of Different Classes of Solid Rocket Propellants

A.K.Sikder N.H. Naik N.H. Naik N.H. Naik V S Mishra V S Mishra R.Vijayalakshmi R.Vijayalakshmi Jatinder Kaur K. P. Vijayalakshmi RM Roy Yogesh Kumar Singh R S Damse Dimple Kumari Ritu Diapuriya P. Srinivasana P. S. Kulkarni PRAVEEN TANDON Charlie Oommen Himanshu Shekhar Himanshu Shekhar

HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune TBRL, VSSC, Chandigarh Thiruvananthapur am HEMRL, VSSC, Pune Thiruvananthapur am DIAT, Pune DIAT Pune TBRL, Chandigarh Periyar University, Salem /HEMRL DIAT, Pune SF Complex, DRDO, Jagdalpur IISc Bangalore HEMRL, Pune HEMRL, Pune

SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCE SCP SCP SCP SCP

Ageing Studies of Composite Solid 168 Rocket Propellants (CSRP) through Uniaxial Tensile Testing Studies on Evaluation of 1,3169 diazidopropane-2-ol (DAPOL) in Gun Propellant Characterization and Synthesis, Formulation 170 Compatibility Studies of DEGDN with Energetic Binders Energy LOVA Gun Studies of Enhanced 171 Propellant Formulations with various Plasticizers of a Fuel Rich Propellant Development 172 Burning at Very Low Pressure Studies on Mechanical Properties of 173 NG-PE-PCP Binder Based Advanced Rocket Propellants Effect of Ballistic Modifiers on NG 174 Plasticized PE-PCP Binder Based Advanced High Energy Propellants Polyurethane based reduced smoke 175 level inhibition system for Nitramine ExtrudedGlycidyl Azide(EDB) propellant Study of Double Base Polymer for 176 Fuel Rich Propellant Applications Studies on Low Temperature 177 Sensitivity Gun Propellant Based on DNDA-57 and Characterization of Preparation 178 nano Fe3O4 and its evaluation in composite propellant formulationsin Study of Fluorocarbon as a Binder 179 Boron Based Fuel Rich Propellant Design Optimization of Cartridge 180 Loaded Composite Propellant PTA Boosteron optimization of NanoStudies 181 Aluminum in Composite Propellant formulation Thermal properties measurement of 182 high energy materials by flash technique NANO PARTICLES IN EFFECTS OF 183 COMPOSITE PROPELLANTS Rationalization of erratic combustion 184 behavior of Nitramine based Composite Propellant Thermal Plasma Synthesized Nano 185 Aluminium Powder for High Energy Applications Polymer Cured with Bis Glycidyl Azide 186 Propargyl Ether of Bisphenol A: Rheological, of Bonding DFT Studies OptimizationThermal andAgents for 187 Different Grain Architecture Thermal decomposition Studies of 188 Ammonium Perchlorate in Presence of Burn rate modifiers activated by

Himanshu Shekhar Sushma Adhav R.Vijayalakshmi RR Sanghavi R. B. Ghavate S M Pande V S Sadavarte MS Mathan JG Bhujbal RR Sanghavi Mehilal Pankaaj Verma S.R. Gore Anjali Kumari R K Kalal Avtar Singh Sitakanta Behera Tanay Seth S.Reshmi Rekha Sangtyani K V.Nimisha

HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune HEMRL, Pune C-MET, Pune VSSC, Thiruvananthapur am HEMRL, Pune VSSC, Thiruvananthapur am

SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP SCP

Thermal decomposition Studies of 189 Ultra fine Ammonium Perchlorate for high burn rate propellants Development of a Smokeless, Single 190 Base Propellant, based on Amino Tetrazole Nitrate - of Nitrocellulose Comparative studyas an alternate to 191 and Guanidinium Azotetrazolate based propellants as pressure generators Development of composite restrictor 192 tube for pyrogen igniter propellant of solid rocket motor Synthesis and characterization of 193 Aluminum nanoparticles obtained using femtosecond laser ablation Studies on new Composite Propellant 194 Formulations with Energetic Ingredients investigation of various Experimental 195 parameters on Mechanical Properties of Solid Propellant Grain Assessment of Safety Zones Based on 196 Dispersion of Toxic Emissions from Rocket Decoring Combustion RemotePropellant System for Solid 197 Rocket Motor Processing Implementation of PLC and Industrial 198 Ethernet based Control System for Solid Composite Propellant Processing Studies on recovery of acetic acid from 199 HMX effluent using Ultra Packed Distillation microflora of soil from pot Studies on Column 200 culture setup using resin based CCC hydrolysate as fertilizer of compost Phytotoxicity assessment 201 end products of 2, 4, 6-Trinitrotoluene (TNT) COMPATABILITY OF ELECTRO 202 EXPLOSIVE DEVICES FOR ELECTRO STATIC DISCHARGE Catastrophe of Breech Blow in High 203 Caliber Guns at Ambient Temperature Study of effuluent treatment during 204 manufacture of some energetic materials Hazard Classification of Propellant SPA205 II Fragment distribution pattern of 206 explosive storage building of 1100kg HD 1.1Analysis for storagePrinciple PSafety based on Unit Risk facility of 207 II system Systematic Safety Approach for 208 Conducting High Calibre Bomb Trials at Testing Ranges Synthesis of TiO2 xerogels for photo 209 oxidation of TNT

Soumyamol B. Hari Hara Nath E.S. Harikrishnan T. Rameshchandran Syed Hamad

VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am VSSC, Thiruvananthapur am ACRHEM, Hyderabad

SCP SCP SCP SCP SCP SCP SCP SHD SHD SHD SHD SHD SHD SHD SHD SHD SHD SHD SHD SHD SHD

Deepak U Deshmukh DIAT, Pune K.Sakthivel S K SAHU Lalatendu Parida Praveen Tandon A. S. Kshirsagar A. U. Chaudhari Ila Tiwari Sandeep Kaur V Anguswamy KS Kulkarni Dr H LYadav Amit Kumar Saini Bimal Kumar S.Thalapathi Raj P. B. Wagh SHAR, ISRO, Sriharikota ITR Chandipur SF Complex, DRDO, Jagdalpur SF Complex, DRDO, Jagdalpur HEMRL, Pune University of Pune University of Pune HEMRL, Pune PXE, Chandipur HEMRL, Pune CFEES Delhi CFEES Delhi CFEES Delhi TBRL, Chandigarh BARC Mumbai

Evaluation Of Suitability Of Ultra-High 210 Speed Fire Detection & Water Based Fire Suppression Systems For Enclosed Safety of operating mechanism of UP 211 Gun in using higher propellant/higher peak pressure in proof testing Experimental Analysis of Propellant 212 Entry into Free Flap in Solid Rocket Motors Management and safe disposal of 213 waste generated during processign solid rocket propellant Hazard Identification and Risk 214 Assessment for Rocket Engines Lightning Risk Assessment and 215 Protection of Structures Housing Explosive Materials VISCO-ELASTIC ANALYSIS OF CASE 216 BONDED PROPELLANT GRAIN FOR ARTILLERY ROCKET for Disposal of A Scientific Approach 217 Waste Explosives in Test Range

ANISH GOPAL V. Anguswamy S K Kumar Amarjeet Kumar N Vijay Shyam Prakash Shelar S.M U N Giri

SF Complex, DRDO, Jagdalpur (ASL) PXE, Chandipur VSSC, Thiruvananthapur am SF Complex, DRDO, Jagdalpur (ASL) DRDL Hyderabad DRDO, Delhi ARDE, Pune PXE, Chandipur

SHD SHD SHD SHD SHD SHD SHD SHD

SCP SCE PTE PT DT DET SHD MQI M&S EMA

Synthesis and Characterisation of Propellants Synthesis and Characterisation of Explosives Performance Testing and Evaluation Pyrotechnics Detection Technologies Detonics Safety, Hazards and Disposal Manufacturing, QA and Inspection Modelling and Simulation Energetic Materials Applications

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