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