oral/poster presentation for hemce-2017hemce2017.org/images/guidelines for poster presentation...3.5...
Post on 20-Mar-2018
268 Views
Preview:
TRANSCRIPT
Oral/Poster Presentation for HEMCE-2017
Instruction to the Authors for Poster
Organizing committee for HEMCE-2017 desires to get all the posters printed locally at Pune,
to maintain uniformity in poster presentations and to manage poster presentations sessions,
effectively. In light of this, following instructions are forwarded to respective authors in connection
with the poster presentations.
1. Each paper selected for poster presentation will be presented using one poster of size 100 cm
height and 70 cm wide.
2. Authors are requested to submit posters in the mentioned size in ready to print condition Power
Point /Corel Draw.
3. All posters will be printed in vertical mode.
4. Poster to include title of the paper (36 point, bold, only first letter of each word capital) in 1 inch
printed size at the top of the poster.
5. Name (30 points, bold, only first letter capital for each word) and affiliation (30 points, italics,
only first letter capital for each word) of the authors/presenters should follow the title of the
paper.
6. The texts in the poster must be readable from minimum 4 feet (120cm) distance.
7. The smallest text in the poster should be 9 mm (3/8”) high in print.
8. The text should be concise enough to be read within 7 minutes.
9. Photo, diagram and graphs should be used to attract attention and should be visible from
minimum 4 ft distance.
10. Flow of the content of the poster should be from TOP LEFT to BOTTOM RIGHT corner.
11. The poster should be made with dark text on light background for good visibility in day time.
12. The texts should not be in all capital letters format. It should be in running text format and all
sub-titles must have first letter capital of the word.
13. In writing texts, use of italics in place of underline is preferred.
14. In main text, use of paragraphs must be avoided and bulleted text is always preferred for better
readability.
15. The poster should be self explanatory for quick assimilation of content and conclusion by the
viewers.
All poster presenters are requested to forward soft copy of their presentation in the above format
to Email (hemce2017@gmail.com) latest by 27th Oct’ 2017, positively. Organisers will not be able
to print the presentation material received after 27th Oct’ 2017 and the responsibility lies with the
presenters to bring the printed material for display.
Instruction to the Authors for Oral Papers
All oral presenters are requested to make presentation material in power point. Tentatively
12-15 mins time is allotted for presentation and 3-5 mins for interaction.
Contact
Dr Himanshu Shekhar Co-Convener HEMCE-2017
Mob : 9422004678 020-25869583 /020-25912283
Email : hemce2017@gmail.com
ORAL PAPERS FOR HEMCE-2017
Paper No.
Paper Serial No.
Topic Estt. /Org
3.4 3 Studies on Effect of non-metallic Fuel on Multispectral Infrared Flare Composition
HEMRL
7.5 8 Studies on Burning Rate of 19-Perf Gun Propellants from Closed Vessel Evaluations
HEMRL
5.2 12 Prospects of Nozzle-less Boosters for Efficient Space Propulsion
SRM Univ
11.7 19 Extension of Shelf Life of Electrically Initiated PAD for Operating Rocket Wrench Mechanism and Water Jet Disruptor System for Ammunition Disposal based on
Experimental Evaluation
ARDE
3.5 20 Experimental Evaluation of Twin Detonator Electro Explosive Device for Initiating Fire Extinguisher System
of Airborne Vehicle
ARDE
11.3 21 Physics of Water-Jet Impingement using Propellant Actuated Cartridge for Improvised Explosive Devices
ARDE
2.4 23 Screening of Boron-Based Solid Fuels for Hybrid Rocket Applications
IIT Kh
5.15 28 Experimental Investigation of Confined Jet Flow Behaviour
SRM Univ
5.3 31 Energetic Composite Solid Propellants for Advanced Space Propulsion
SRM Univ
5.4 32 Study on Improvement of Regression Rate and Combustion Efficiency in Hybrid Rocket Motor Using
Multi-Protrusion
BITS Ranchi
10.2 34 ISROSENE-Aluminum Gel propellants - Synthesis and Rheological Characterization
VSSC
5.1 35 Improvement in Performance of Solid Rocket Motor by Modifying Grain Configuration
RCI
7.4 36 Nitrogen Rich Compounds: An Approach to Reduce Gun Barrel Erosion
HEMRL
10.1 42 Pressure Induced Changes in TEX Studied by X-ray Diffraction and Raman Spectroscopy: Implications on
Explosive Properties
IGCAR
2.6 44 3D Numerical Investigation of Hydrogen Combustion in a SCRAMJET to Enhance Combustion Efficiency
BITS Ranchi
3.3 46 Qualification of Ignition Initiation System for Large Solid Rocket Motor
ASL
5.7 47 Design Optimization of Star Grain for Solid Propellant Rocket Motor
CHESS
5.8 52 Development of High Burning Rate Composite Propellant for Nozzleless Booster Application with
Enhanced Strain Capability
HEMRL
5.11 56 Development of Nano-Aluminium Based Composite Propellants by Tailoring Diol-Triol Content and [-
NCO]:[-OH] Ratios
SFC Jagdalpur
5.9 57 Investigating the Effect of Injector Type on the Regression Rate of the Hybrid Rocket
BITS Ranchi
9.2 59 Development of Surface Enhanced Raman Spectroscopic Substrates for Detection of Explosives
IISc
13.5 61 Surface Coating over Fine and Ultrafine Ammonium Perchlorate
VSSC
1.2 70 Synthesis and Characterization of Propyl Nitroguanidine (PrNQ): An Insensitive Energetic
Material for Melt-Cast Formulation
HEMRL
1.5 71 Studies on Compatibility & Storage Stability of Cyanuric Triazide (CTA): A Lead-Free Primary Explosive
HEMRL
11.5 72 Toxicity Evaluation of UltraFine HMX on Triticum sp., Human Skin (HaCat) and Lung Cells (L-132)
SPPU
8.2 74 Structural, Elastic and Electronic Properties of Crystalline Bis (nitrofurazano) Furazan (BNFF-1) using
Van der Waals Density Functional Approach
ACRHEM
5.6 75 Effect of Binder Melt Flow on the Leading Edge Flames of Solid Propellant Sandwiches
ACRHEM
7.3 76 Performance Evaluation of Base Bleed Motors for Artillery Projectile under Dynamic Conditions: an
Innovative Approach
PXE
10.9 82 Laser Doppler Velocimetry Technique for Determining Instantaneous Burning Rate and Response Function of
Solid Propellants under Fluctuating Pressures
ITM
1.4 83 Preparation of Low Aromatic and Ultra-Low Sulphur Jet Fuel for Air-Breathing Engine Applications
CPCL Chennai
4.1 85 Aluminium Hydride Synthesis by Electrochemical Route
ARCI
9.1 86 Standoff Detection and Classification of Explosive Molecules Using Femtosecond LIBS
ACRHEM
4.11 97 Synthesis of energetic oxidizer bis(2,2,2-trinitroethyl)amine (BTNA) and theoretical
performance evaluation as a propellant ingredient
ACRHEM
12.4 99 Synthesis and Characterization of Al-Mg Eutectic Nanoalloy Particles by Electrical Wire Explosion
Process
IITM
8.1 100 Application of the Methodology “Counterflow Diffusion Flames” in Modeling of the Terminal Ballistic Processes of Munitions Based on Reactionary Material
RUSSIA
12.2 101 Fabrication of Nano/Micro-Explosive Particles in Liquid Media using Femtosecond Ablation Technique
ACRHEM
11.6 104 Ammunition Dismantling System with customizable Caliber / Geometry for various ammunitions
HEMRL
10.8 106 Shadowgraphy Imaging of Laser Induced Shockwaves in Transparent Media
ACRHEM
10.3 107 Amphiphilic Polymer Modified Graphene Surfactant: Effect on Thermal Stability and Mechanical Properties
of Carboxylated Nitrile Latex Nanocomposites
IICT
8.3 108 Numerical Simulation of Laser Induced Shock Waves from Aluminum film in Presence of Helium Gas at
Different Ambient Pressures
ACRHEM
4.2 109 Real Time Analysis of Crystallization Process Dynamics of NTO using FBRM & PVM
HEMRL
13.3 110 Studies of Parametric Optimization and Reaction kinetics of precursors of DNDA-57, an Energetic
Plasticiser
HEMRL
11.4 116 Modelling of Safety System and Comparison of Safety Systems between Government and Private
Organizations
VSSC
3.6 124 Development of MEMS Pyrotechnic Thruster for Micro Propulsion Applications
VSSC
8.4 125 Pressure Estimation for Pyrotechnic Devices Using Energy Based Mathematical Model
VSSC
10.10 126 Optimization of Interface Properties of Composite Propellant with NBR Insulator based on the Studies on
Liner Thickness and Casting Time
ACEM
6.3 127 Effect of Particle Size of Aluminium on Pressable Plastic Bonded Explosives
HEMRL
8.5 130 Quantum-Chemical Studies on 7H-[1,2,4]Triazolo[4,3-b][1,2,4]Triazole Containing Energetic Salts
NITK
8.8 131 DFT Studies for Rate Constant Computation of Aromatics and Heterocycles Nitration in Mixed Acid
Environment for High Energy Materials Synthesis
HEMRL
13.4 132 Reaction and Reactor Engineering of Bachmann Process for RDX Production
HEMRL
4.12 133 Studies on Friction Insensitivity Improvement of Tetranitroacetimidic Acid
HEMRL
11.2 140 Investigation of Suitability of Chemical and Electro-Chemical Treatment Methods for Destruction of Perchlorate in Solid Propellant Hog-Out Effluent
SFC Jagdalpur
10.11 144 Assessment of Mechanical Properties of Aged Composite Propellant by Indentation Method
HEMRL
4.4 145 Preparation of Energetic Composite Material Containing Boron Aluminium Ligature (BAL) and FOX-7
HEMRL
4.3 146 Single-Step Catalytic Conversion of Isopentane into Isoprene
IIP Dehradun
13.6 151 Studies on Effect of Screw Geometry and Operating Conditions on Residence Time Distribution in a Twin
Screw Continuous Mixer
HEMRL
10.4 152 Studies on Effect of Propellant Formulation on Pseudo-plasticity, Thixotropicity and Yield Stress
HEMRL
3.2 155 Application of Ultrafine e-CL-20 Explosive in Slapper Detonator
TBRL
7.2 159 Effect of Dinitrodiaza Alkane as Energetic Plasticizer for Extruded Double Base Propellant Formulations
HEMRL
12.3 168 Cotton Assisted Hydrothermal Synthesis of Nano Copper Oxide : Promising Catalyst for Ammonium
Perchlorate Thermal Decomposition
VSSC
8.6 169 Computational Studies on Combustion Instability of Solid Rocket Motor: A Case Study
IITM
6.4 176 Use of Pyral Powder to Increase the Yield of Explosives IITM
4.10 179 Effect of solvent polarity and temperature on recrystallised ammonium perchlorate
VSSC
11.1 181 Development of Construction Materials for Explosive Storage Buildings
CFEES
8.9 182 Understanding the Sensitivity of Explosive Crystals: A Computational Approach
HEMRL
8.7 185 HEM Screener: A Chemoinformatics Tool for Design and Development of Novel High Energy Materials
Using Virtual Screening
NCL
9.4 187 Identification of Explosives using Standoff LIBS Combined with Multivariate Analysis
ACRHEM
2.7 190 Frequency time analysis of pressure time profile of solid rocket motors having combustion instability
HEMRL
10.5 191 Propellant Burning Wave Studies by Embedded Thermocouple and Imaging Method at Ambient
Pressure
HEMRL
7.1 192 Active Propulsion of an Artillery Gun Shell by Means of A RAMJET
IITM
5.5 196 Performance study of Aluminum Based Water Ramjets
IITM
13.1 197 Boron Aluminum Ligature (BAL) Obtained using DC Thermal Plasma Route and Their Thermal Properties
SPPU
10.7 199 Optimization of Regression Rate of Solid Fuel Grain in Hybrid Rocket Motor by Vortex Generation
PCOE
5.12 202 Failure Analysis of the Propulsion System for Antitank Guided Missile (ATGM)
HEMRL
9.3 204 Temperature Dependent Terahertz Spectroscopy of Aqueous Soluble and Insoluble Explosives
ACRHEM
4.13 208 Optical Absorption in Metal Nanoparticle Doped High Energy Material Composites
ACRHEM
9.5 213 Design and Development of Automated Gun Propellant Metrology System
HEMRL
6.5 214 Studies on Detonation Reliability of High Explosive Booster for a Specific Application
VSSC
4.6 218 Synthesis and Characterization of Energetic Polyphosphazene
HEMRL
3.1 219 Development of a PETN Based SDT Detonator Using ZPP as an Initiating Charge
VSSC
10.12 222 False Positive Indications in the Digital Radiograph of Warhead due to Scattering of X-rays
HEMRL
13.2 225 Particle Size Reduction of b-HMX by Nozzle Assisted Spraying
TBRL
11.8 234 Microbial Remediation –A Potential Green Technology for Treatment of Energetic Chemicals Present In
Wastewater and Soil
CFEES
11.9 238 Innovative Design of Multi-compartment Propellant Storage Building
CFEES
8.12 242 Role of Thermal Conductivity in Determining Temperature Sensitivity
IITM
5.13 252 Production Oriented Sleeve Cast Inhibition Technique for Cartridge Loaded Composite Propellants
HEMRL
12.5 255 Synthesis of High Surface Area Copper Oxide Nano Flower and its Application as Burning Rate Modifier in
Composite Propellant Formulation
HEMRL
8.10 257 Experimental and Numerical Studies on Initiation Behavior of Thin Explosive Sheets on Impact of Shaped
Charge Jet
HEMRL
4.7 259 Synthesis and Characterization of BPTAP: As Alternative Heat Resistant Explosive
HEMRL
4.8 269 Nitro-Functionalized-Hydroxyl Terminated Polybutadiene: A Potential Energetic Polymer for
Composite Propellant
HEMRL
6.2 272 Evaluation of Layered Fuel Rich Explosive Charges for Thermobaric Applications
HEMRL
1.6 273 A patent review on Green Materials in HEMs / Munitions
CSIR-URDIP
1.3 275 Studies on Effect of RDX Quality on the Shock Sensitivity of Polymer Bonded Explosive Formulations
HEMRL
10.6 276 3D X-Ray Computed Tomography (3D-CT): Inspection Technique for Comprehensive NDE of Explosive
Systems
HEMRL
5.14 279 Design of Ignition System for Nozzle Less Booster (NLB) Motor
HEMRL
6.1 280 2,4,6- Triamino-1,3,5-Trinitrobenzene Based Explosive Formulations Containing Vinylidene Fluoride-
Chlorotrifluoroethylene Copolymers Matrices with Different Molecular Weight
TBRL
2.5 281 Gaseous Hydrocarbon Combustion Studies in High Pressure Rocket Combustors
IITK
2.3 282 Investigation of Reverse Flow Slinger Combustor IITK
8.11 283 Explosively Driven Hyper Velocity Launcher TBRL
4.9 287 Effect of Relative Humidity on Flow Properties of Dry Coated Fine and Ultrafine Ammonium Perchlorate
Powder
ACEM
4.5 293 Microwave Assisted Synthesis of Glycidylazide Polymers-Triol (GAP-Triol) Using Polyepichlorohydrin-
Triol (PECH-Triol) as an Energetic Polymer
NMU Jalgaon
12.1 299 Preparation and Characterization of Nano HNS TBRL
2.1 303 Research on Solid Propellant Burning Process in Low Temperature Gas Generator
RUSSIA
1.1 304 Sublimation and Thermal Decomposition Kinetics of 1,1-Diamino-2,2-Dinitroethene (FOX-7)
RUSSIA
5.10 306 Self-Organized Micro-Scale Oscillatory Systems of the Reactionary Zones and Concept of the Smart Solid
RUSSIA
Micro-Propulsion System
2.2 307 Artificial Neural Networks Models of Energetic Materials Combustion
RUSSIA
4.14 309 Spectral Properties of Energetic Materials and their Heating by the Near-IR Laser
RUSSIA
POSTER PAPERS FOR HEMCE-2017
Paper No. Paper Serial No.
Topic Estt. /Org
P11.1 1 Risk Assessment of RF Hazards in Test Range ITR,Balasore
P3.1 2 Effect of Binders on Burning Rate of Slow Burning Tungsten Based Pyrotechnic Delay Composition
HEMRL
P3.2 4 Effect of Particle Size of Magnesium on Performance of Magnesium / Teflon / Viton (MTV) Flare
Composition
HEMRL
P10.1 5 Thermal Studies on Gun Powder with Low Combustion Residue
HEMRL
P8.1 7 Simulation of Free-Field Incident Blast Over-Pressure Curves at Intermediate Scale Distances
HEMRL
P 2.1 10 Final Stratified Premixed Combustion in Gas Turbine Engines
SRM Univ
P5.1 11 Comparison of Performance Parameters for Different Bore Configurations
SRM Univ
P6.1 14 Studies on Dispersion Pattern of Incendiary Cinders HEMRL
P3.3 18 Studies on Effect of Epoxy Binder on Sensitivity of Red Phosphorus based Smoke Compositions
HEMRL
P11.2 22 Design and Testing of Electro Explosive Devices for Water-Jet Disruptor Application
ARDE
P5.2 25 Platonisation of Nitramine Based Extruded Double Base Propellant
HEMRL
P5.3 26 Accelerated Temperature Ageing Studies on High Burn Rate Extruded Double Base Propellant
HEMRL
P10.2 27 Thermal Degradation Behaviour and Effect on Thermal Properties of Charring Ablators
ASL
P 2.2 29 Effect of Particle Size on Droplet Regression, Break-up and Combustion Characteristics of Boron-Laden
Jet Fuel Droplet
IIT Kh
P8.2 37 Finite Element Modelling of Heat Transfer and Cure analysis in Polymer Composites
VSSC
P8.3 38 Numerical Modelling of Seasonal Climate Temperature Influence on The Performance of Solid
Rocket Motor
VSSC
P6.2 39 High Explosive Based Single Fragment Launcher at Hypervelocity
ARDE
P10.3 40 Identification of TNSTAD (trans- 1,4,5,8 -tetranitrosotetraaza decalin) as a Substitute for Picrite in Unknown Triple Base Gun Propellant
HEMRL
P8.4 41 Electronic properties and Hirshfeld surface analysis of Dihydroxylammonium 5,5'-bistetrazole-1,1'-
diolate under pressure
ACRHEM
P8.5 43 Theoretical Predictions of Novel N-nitramines for their use as High Energy Materials
DIAT
P5.4 49 A Study on Grind ability of Revised AP Feed Fraction to Achieve Specified AP fine Particle Size Distribution
and Ballistic properties of Agni Motor
SDSC
P12.1 50 Energetic Nano-composite as a Coating Material for Desensitization of High Energy Materials
HEMRL
P4.1 51 Development of HTPB based Polymer Clay Nanocomposite as a New Binder System for
Composite Propellant
HEMRL
P8.6 58 A Theoretical Study on Improved Energetics of nano-Aluminized Composite Propellants with GAP based
AP/ADN Formulations for Rheological Feasibility
SFC Jagdalpur
P4.2 62 Synthesis, Spectral Analysis of some 5-nitro-1-aryl/alkyl-tetrazoles
ANNAMALAI Univ
P4.3 63 Synthesis and Characterization of Aluminium Hydride
ANNAMALAI Univ
P4.4 64 Synthesis and Characterization of α -Nitrolactone: Monomer for Energetic Binder
ANNAMALAI Univ
P4.5 66 Synthesis and Characterization of Isowurzitane and Tetrazole Crafted HTPB
ANNAMALAI Univ
P11.3 67 Safety challenges in handling raw materials for solid propellant production
VSSC
P12.2 68 Nano Aluminium - Synthesis, Characterization and Ballistics Study
VSSC
P10.4 73 Model-Free Approach on the Thermal Decomposition Kinetics of an Energetic Ionic Liquid:
1-Methyl-4-Amino-1,2,4-Triazolium Nitrate
VSSC
P5.5 77 Instantaneous Burning Rate Measurement of Plateau and Non-Plateau Propellant Using Ultrasound
Technique
IITM
P5.6 78 Combined Effect of Paraffin and Microcrystalline Wax on Mechanical Properties and Regression Rate
of the Hybrid Rocket Fuels
BITS Ranchi
P9.1 79 Centrifuge Testing: An Indispensible Quality Control Tool to Examine and Improvise Interface and
Structural Integrity of Large Size HEM based System for Ensuring High System Reliability
SFC Jagdalpur
P5.7 81 Measurement of Pressure Coupled Combustion Response of a novel Composite Solid Propellant by
Pulsed T-Burner Method
RIC Chennai
P5.8 84 Formulation Studies and Performance Verification of a new Pyrotechnic Igniter Composition for Ballistic
Evaluation Motor (BEM)
VSSC
P4.6 88 Identification and Quantification of Unknown Two Component Liquid Explosive
HEMRL
P12.3 89 Ag-Au Bi-metallic Nanoparticles and Nanostructures Fabricated by Femtosecond Laser Ablation for
Detection of 2- 4 Dinitrotolune
ACRHEM
P8.7 90 Study on the Effect of Gap Between the Ballistic Evaluation Motor and Assembly Chamber on
Propellant Burning Rate Prediction
SDSC
P12.4 91 Synthesis and Characterization of Sb2S3
Nanoparticles for Pyrotechnic Delay DIAT
P8.8 92 Different Methods for Simulating High Altitude Testing of Rocket Motors
ACEM
P8.9 93 Correlation of Sub-Scale Rocket Motor Burn Rate with Strand Burn Rate for Different Burn Rate
Compositions
ACEM
P10.5 95 Monitoring of Degradation of Methylene Blue Dye by MEMS Technology
HEMRL
P12.5 96 Catalytic Decomposition of Ammonium Dinitramide –Water Liquid Propellant by Free Standing CuO
Nanoparticles
ACRHEM
P10.6 98 Thermal Decomposition Kinetics of a Potential Oxidizer Tetranitroacetimidic Acid (TNAA)
ACRHEM
P4.7 102 Quantification of 4-(1- hydroxymethyl)-2,2-Dimethyl-1,3-Dioxalane (C3) and 4-(2- Hydroxyethyl)-2,2-
Dimethyl-1,3-Dioxalane (C4) by Gas Chromatography
HEMRL
P5.9 103 Studies on TKX- 50: Preparation of Different Particle Size and its Effect on Ballistic Properties in HTPB/AP/Al based Composite Propellant
Formulation
HEMRL
P10.7 105 Interface Bond Strength Evaluation System for Combustible Cartridge Case (CCC) based Tank
Ammunition
HEMRL
P13.1 111 Process Development for preparation of Fine Ammonium Perchlorate by Recrystalization in a
Batch Mode
HEMRL
P13.2 112 Development of Continuous Methodology for Preparation of Fine AP, an Oxidizer for Propellant
Formulations
HEMRL
P13.3 113 Process Development and Scale-Up of Reduced Sensitivity-RDX
HEMRL
P13.4 114 Process Optimization for preparation of N,N’- Dinitro– N, N’ – Dimethyloxamide
HEMRL
P11.4 115 Study of Sound Level in Crew Area for Large Caliber Artillery Gun fitted with Double Baffle Muzzle Brake
ARDE
P11.5 117 Analytical Study of Safety through Differential Equations
VSSC
P11.6 118 Removal of Perchlorate from Water Using Iron Doped Activated Carbon - Sustainable Adsorbent
VSSC
P10.8 119 Activation Energy and Kinetics of Oxidation of Amorphous Boron Powder and Aluminium
Dodecaboride
HEMRL
P10.9 120 Oxidation and Kinetic analysis of Aluminium Diboride HEMRL
P11.7 122 On the Feasibility of Jetfans for Aircraft Fire Safety SRM Univ
P10.10 123 Linear Charge Off-Set Studies on RDX Based Flexible Linear Shaped Charge (FLSC) by Using NDT
Techniques (X-Ray & NR)
VSSC
P10.11 128 Quantification of Curing Agent in HTPB-TDI Base Liner Composition used in Case Bonded Composite
Propellants
HEMRL
P6.3 129 Comparative Studies on Tungsten & Aluminium loaded Pressable Plastic Bonded Explosives
HEMRL
P5.10 134 Quantification of Binder Melt in Composite Solid Propellants
IITM
P5.11 135 Thermal, Ballistic and Rheo-Mechanical Characterization of High Burn Rate Composite Solid
Propellant for Crew Escape System
VSSC
P5.12 136 Studies on Effect of Boron – Aluminium Ligature (AlB12) on the performance of Boron – Potassium
Nitrate Igniter Composition
HEMRL
P6.4 138 Challenges to build Multiple Scarfed Nozzle Jettisoning Motor for Crew Escape System
VSSC
P13.5 139 Analysis of ABP Process Effluent and Design of Treatment Plant
HEMRL
P6.5 141 Experimental Comparative Study of Ground Burst and Stand-Off Burst during Measurement of Blast
Pressure Parameters of Explosives
HEMRL
P6.6 142 Experimentation and Analysis for Estimating Explosives Fireball Parameters using Scaled Weight
Method
HEMRL
P10.12 147 Studies on Effect of Particle Size of Ammonium Perchlorate on Impact, Friction and Spark
Sensitivities
HEMRL
P8.10 148 Modelling of Size Reduction Operation of Ammonium Perchlorate in Hammer Mill
HEMRL
P5.13 150 Studies on Development of Potassium Perchlorate based High Energy Extruded Double Base Propellant
HEMRL
P13.6 153 Design of Slurry Distributor and Cone for Casting of Propellant Slurry for Complex Rocket Motor
HEMRL
P8.11 154 Exploring the Compatibility of Energetic Plasticizer DNDA-5 with Energetic Binders: Thermal and DFT
Study
HEMRL
P4.8 156 Preparation, Characterization and Threshold Initiation Studies of Ultrafine RDX
TBRL
P6.7 157 Studies on Fluoro polymer Based Plastic Bonded Explosive Compositions
HEMRL
P10.13 158 Accelerated Ageing of Solid Propellants: A New Approach
IITM
P4.9 160 Synthesis and Curing Behaviour of Non-Isocynate Binder: Poly (Allyl Azide)
HEMRL
P4.10 161 Compatibility Study on Poly (Allyl Azide) vis-a-vis Explosive / Propellant Compositions
HEMRL
P10.14 163 Evaluation of Thermal Stability of Composite Propellants with Varying Coarse to Fine Ammonium
Perchlorate Ratio and Catalyst Concentration
VSSC
P8.12 164 Model for Determination of Detonation Properties of C-H-N-O Based Halogenated Polymer Bonded
Explosives
TBRL
P4.11 166 Novel Spectrophotometric Method for Determination of Hexavalent Chromium in
Composite Solid Propellants
VSSC
P11.8 167 Disposal of Unserviceable Ammunitions of Different Hazard Divisions (HD) using Innovative Methods
TBRL
P11.9 171 Studies on Removal of Peroxide in Effluent from HTPB Plant
VSSC
P6.8 172 Vibration Casting of Highly Viscous Composition of HMX: TNT
TBRL
P3.4 173 Development of a Pyro-based Isolation System for High Altitude Engine Tests
VSSC
P7.1 174 Study on DEGDN Based High Performance Gun Propellant for Tank Gun Ammunition
HEMRL
P5.14 175 Optimization of Solid Loading for Processing of Nitrate Ester Plasticized Polyester Polyol based
Advanced Energetic Solid Rocket Propellants
HEMRL
P13.7 177 Design of Nozzle for Spray Atomization Process for Recrystallization of Ultrafine Explosives
TBRL
P5.15 178 Studies on Burn Rate Modification of Advanced Energetic Solid Propellants
HEMRL
P7.2 180 Development and Evaluation of High Energy Nitramine Based Gun Propellant Composition
HEMRL
P8.13 183 A QSPR Based Method for the Prediction of Heat of Combustion of Diverse Higher Energy Materials
Using Partial Least Square Regression and Genetic Programming
NCL
P8.14 184 MD Simulation Studies on HTPB-b-GAP Copolymers HEMRL
P4.12 186 Synthesis of Nitro Substituted 1, 2, 4-Triazole, Imidazole and Alkylnitramine Derivatives: A New
Class of Energetic Materials
HEMRL
P8.15 188 Prediction of Electrostatic Spark Sensitivity of Energetic Molecules (CaHbNcOd) by Artificial Neural
Network
HEMRL
P9.2 193 Quality Control Tools for Linear Explosive Cords VSSC
P6.9 195 Studies on Surface Coating of HMX with TNT and Polymer Binder
TBRL
P5.16 198 Validation of Burn Rate Law for Composite Igniter Propellant at Higher Pressures
VSSC
P6.10 200 Process Optimization of Isostatically Pressed PBX Based Shaped Charge Using Taguchi Approach
TBRL
P10.15 201 Compatibility Study of Octahydro- L, 3, 5, 7-Tetranitro- 1, 3, 5, 7-Tetrazocine with Energetic
Materials and Inert Polymeric Materials
TBRL
P11.10 203 Assessment of Environmental Parameters of NHN Effluent and its Disposal
HEMRL
P8.16 205 Lattice Dynamics and Thermodynamic Response of Cubic Alkaline-Earth Metal Nitrates M(No3)2 (M= Sr,
Ba): A First Principle Study
ACRHEM
P9.3 206 Quality Assurance of Military Explosives : An Overview
CQA(ME)
P10.16 207 Kinetic Evaluation of Zirconium/Potassium perchlorate (ZPP) as Primary Charge of ISRO
Standard Initiator
VSSC
P10.17 210 Designing of a Corrugated Acoustic Spectrum Analyzer for Characterization of Laser Induced Shock
Waves from Solid Graphite
ACRHEM
P4.13 211 A Rheological Method to Measure the Degree of Exfoliation of PU/Clay Nanocomposite
HEMRL
P5.17 212 Study of Bonding Agent cum Surfactant on Composite Propellant
HEMRL
P10.18 215 Radiography of Planar Defects in Gas Generator (GG) Grains
HEMRL
P5.18 216 Determination of Long Term Strain Endurance Capability of HTPB Based Solid Propellant
VSSC
P4.14 217 Rapid determination of Boron content in Amorphous Boron Powder (ABP) using Atomic Spectrometry
HEMRL
P8.17 220 Investigation of Dual Bridgewire Detonating Cartridge Anomaly through Numerical Analysis
VSSC
P3.5 223 Ignition and Thermal Behavior of Al/MoO3 Thermite for LASER Ignition Application
HEMRL
P10.19 224 Study of Radiographic Image Quality Achieved on Film for an Explosive Charge Using 7 MeV X-Rays
TBRL
P11.11 226 Recycling Hazardous Waste of Combustible Cartridge Case High Energy Materials into Crop Fertilizer by
the Process of Alkaline Hydrolysis
DIAT
P10.20 227 Study on Shelf Life and Ageing Characteristic of Pedcoat Liner used in Processing of Large Size Solid
Rocket Motor
SFC Jagdalpur
P11.12 230 Hazards of TNT Exudation and Preventive Measures CFEES
P11.13 231 Issues and Challenges of Demilitarisation of Ammunition in India
CFEES
P11.14 232 Static Electricity : Hazards in Explosive Environment and Remedial Measures
CFEES
P8.18 233 Correlation for Propagation of Blast Waves in Tunnel CFEES
P10.21 236 Study on Factors Affecting Propellant –Rubber Peel Strength in Processing of Large size Solid Rocket
Motors
SFC Jagdalpur
P6.11 237 Underground Explosion and Propagation of Ground Shock
CFEES
P11.15 239 Sacrificial Protective Wall for Impulsively Loaded tructure
CFEES
P10.22 240 Study Effect of Aging and Temperature on Creep Deformation of Epoxy Resin, Applying Method of
Accelerated Aging
SFC Jagdalpur
P12.6 241 Zero Valent Iron Loaded Silica Nanoparticles for the Removal of TNT, DNT, HMX and RDX
CFEES
P13.8 243 Synergetic Approach towards Utilization of Effluent of TATB Pilot Plant for Effective Leaching of Crude
Amorphous Boron Powder
HEMRL
P4.15 244 Study on Quantitative Analysis of Copper Chromite in Composite Propellant Using Inductively Coupled
Plasma-Optical Emission Spectroscopy-An Instrumental Method
SFC Jagdalpur
P4.16 245 Synthesis and Characterization of Polyglycidyl Ethers: An Isocynate Free Curative
HEMRL
P11.16 246 Studies on Conversion of Waste Fuel Rich Based Propellants into Liquid Fertilizer and its Effect on
Plant Growth
HEMRL
P5.19 247 Hydroxyl Terminated Polybutadiene Based Machinable Polyurethane Inhibition System for Solid
Rocket Propellant
HEMRL
P8.19 248 Design and construction of Radial Hole Drilling fixture for HELINA Nitramine Extruded Double Base
Propellant
HEMRL
P4.17 249 Unique Liner Formulation for processing of case Bonded Rocket Motors
HEMRL
P10.23 250 Studies on effect of Nano Clay in Inhibitor Formulation for Inhibition of Gas Generator
Propellants
HEMRL
P4.18 251 Development of Bonding Promoters for Silicone Based Insulation with HD1.1 Class of Propellant
HEMRL
P8.20 253 A Simplified Mathematical Model for Predicting Performance of Low Explosive Charges
VSSC
P11.17 254 Significance of Operational Hazards in Propellant Manufacturing
CFEES
P10.24 256 Studies on Evaluation of Ferric Citrate in HTPB/AP/Al Composite Propellant Formulations
HEMRL
P8.21 258 Design and Development of Delay Module for Triggering Combustion Instability
HEMRL
P10.25 261 Image Processing Tools and Algorithms for Assisted Defect Recognition (ADR) in Digital Radiograph of
Propellant Grains
HEMRL
P5.20 262 Studies on the Effect of Ammonium Perchlorate (AP) Particle Size on the Mullins Effect Phenomena in
Composite Propellants
ACEM
P10.26 263 Experimental and Flory a-Model Based Characterization of PBPU Elastomer in Composite Propellant Applications and Fitting of Molecularly
Derived Rubber Elasticity Models
ACEM
P10.27 264 Challenges in Solid Rocket Motor Radiography HEMRL
P8.22 265 Atomistic Molecular Dynamics Simulations of Hydroxy Terminated Polybutadiene (HTPB) on
Aluminium Surface
ACEM
P8.23 267 CFD Analysis of High Pressure and Temperature Gases in Multi Propellant Grain Rocket Motor
HEMRL
P5.21 268 Effect of Propellant Burn Rate on Performance of an Artillery Rocket
ARDE
P4.19 270 Analysis of Variability of Instrumental Determination of Composite Propellant Properties
ACEM
P10.28 271 Study on Optimization of Catalyst Concentration to Reduce Curing Time of Inhibition Resin
ACEM
P3.6 274 Studies on Thermal Behavior of LFCN/KClO4/Viton Pyrotechnic System
HEMRL
P6.12 277 Blast Pressure Attenuation in Woollen Felt TBRL
P5.22 284 Feasibility Study of Indigenous Amorphous Boron Powder (ABP) of purity 91-93% in igniter
composition
HEMRL
P5.23 285 Design of Ignition System for Booster motor of Pilotless Target Aircraft (PTA)
HEMRL
P5.24 286 Analysis of Factors Affecting Web Thickness of Ballistic Evaluation Motor
ACEM
P4.20 288 Rapid and selective Analysis of High Energy Propellant Ingredients by Reverse Phase HPLC
method
HEMRL
P8.24 289 Prediction of Detonation Velocity of Polymer Bonded Explosives by Using Empirical Approaches
HEMRL
P6.13 290 Effect of Tungsten Content on Metal Acceleration Properties of Polymer Bonded Explosive
Formulations
HEMRL
P6.14 291 Study of effect of blast wave generator parameters on blast wave strength
TBRL
P8.25 292 Assessment of Performance of Various Polymers in HMX and TATB Based Polymer Bonded Explosives
(PBXs) for its Long Term Storage Applications
TBRL
P4.21 294 Synthesis and Characterization of Poly(Allylazide-Tetrazole) (PAAT) As An Energetic Polymer
NMU Jalgaon
P5.25 295 Propellant - Inhibition Interface Bonding - HTPB Based Composite Propellant
ASL
P6.15 296 Interaction of a Shock Tube Generated Blast Wave with Solid Obstacles
CSIR-CMERI
P10.29 297 Enhancement in Burn Rates of Composite Propellant Using High Surface Area Pyral Al: An Approach for
Achieving Higher Shelf Life
SFC Jagdalpur
P10.30 298 Development of Viscoelastic Stress Analysis Capability for Structural Integrity Assessment of Solid
Propellant Grains
VSSC
P6.16 300 Effect of Fluoro and Silicone Based Polymeric Binder on Impact and Friction Sensitivity of High Explosives
TBRL
P10.31 301 Study on Accelerated Ageing of HMX, Viton and their PBX by Vacuum Stability Thermal Testing
TBRL
P 1.1 305 Experimental Investigation of Slow Cook-Off for IM Compliance
TBRL
P4.22 308 Synthesis, characterization and performance study of inorganic high energy nanocomposites materials
OFB Bolangir
top related