| Binder | Non-isocyanate based cure binder system propellant | HEMRL |
| Booster | High performance large size booster | ASL |
| Nozzle Less Booster for Long Range Air to Air Missiles | DRDL |
| Compact Engine | High specific power, compact and lightweight engines for aero application (200 hp to 300 hp) | VRDE |
| Control Systems | Compact Agile Divert Attitude Thruster Control System | DRDL |
| Digital Twin | Digital Twin Technology for Structural Integrity evaluation for propulsion systems | ASL |
| Dry Engine | Flight worthy Aero Engine for Unmanned Combat Air Vehicle | GTRE |
| Electric Propulsion | Air Breathing Electric Propulsion for Very Low Earth Orbit (VLEO) | - |
| Electric Propulsion for Air Ship | ADRDE |
| Electrically Throttlable Propellants | Electrically ignitable propellant and its ability to throttle and control of burning rate with electrical parameters | HEMRL |
| Explosive Disposal | Technologies for safe disposal of propellants | HEMRL |
| Fuel Management | Fuel Flow Controller for Long Range Air to Air Missiles | DRDL |
| Fuel flow controllers for liquid/air breathing propulsion systems for Ramjet Thrust Modulation - Pulse Width Modulation Valves & Flow Controllers | DRDL |
| Gas Generator | Advanced Turbo Gas Generator for Anti -Ship Cruise Missile | GTRE |
| Gas Generators for System articulation | ASL |
| On-board N2 Gas generator | ASL |
| Steam Gas generators for Canister applications | ASL |
| Gas Turbine Engine | Digital Engine Control Unit for Small Turbo Fan Engine | ADE |
| Fuel Flow Metering Unit for Fighter Aircraft with form fit replacement | ADE |
| Gas Trubine Engine | GTRE |
| Long Endurance Small Turbo Fan Engine | GTRE |
| Small Turbo Fan Engine For Air Launched Cruise Missile | GTRE |
| Jet Propellor | Constant Speed Propellers | ADE |
| Life Cycle Assessment | Accelerated ageing studies on composite solid propellants | DRDL |
| Characterize the viscoelastic nature of propellant using accelerated ageing studies to understand the behavior of propellant during its lifecycle | HEMRL/ACEM |
| Sample evaluation for natural ageing and Statistical model incorporating Artificial Intelligence framework using ANN, ML and DL | HEMRL/ACEM |
| Liquid Propulsion | Regen Cooled Engine - Liquid Propulsion (LP) for Liquid Upper Stage for High Altitude Interceptor | DRDL |
| Variable Thrust Engine 40% to 100% for Thrust Modulation - Flow Controller | DRDL |
| Mono-Propellant for Reaction Control System & Satellite Propulsion - Hydrazine Based Thrusters | DRDL |
| Regen Cooled Engine for Liquid Upper Stage Rocket Engine | DRDL |
| Surface Tension based Propellant tanks | DRDL |
| Liquid Propellant Based Ballistics Charaterization for High Mach Muzzle Power Travelling Charge System Gun | ARDE |
| Materials | Rocket Motor Casing using Steel Strip Technology with Insensitive Munition (IM) compliance | NMRL |
| Alloy for Gas Turbine Blade | DMRL |
| High Performance Carbon Fibre for Composite Rocket Motor Casing | ASL |
| Hydroclaved Carbon Phenolic for large Solid Rocket Motor throat | ASL |
| Light Weight Ablative liners | ASL |
| Resins compatible to high strength fibres | ASL |
| Propellant | Advanced Energetic smokeless propellants | HEMRL |
| Advanced Propellant formulations with high specific impulse for different applications (Aluminised and non-aluminised) | HEMRL |
| Alternate fuels (Bio fuels / blended fuels ) | CVRDE |
| Ammonium Dinitramide for realizing higher specific impulse | HEMRL |
| Boron based composites and bimetals as attractive fuel additives for application in explosive and propellants, thermites, igniters | HEMRL |
| Different burn rate based on the thrust requirements | HEMRL/ACEM |
| Double Base Propellant with less Flame temp | HEMRL |
| Endothermic Fuel for Long Duration Hypersonic Engines | DRDL |
| Extruded Fuel Rich Propellant in Ramjet mode | HEMRL |
| High Burn Rate propellant for Gas Generators | ASL |
| High energy density fuels using plant metabolites | DIHAR/DIBER |
| Manufacturing technology for key burning rate modifier, Butyl ferrocenesilane grafted Hydroxy Terminated Polybutadiene (HTPB) | HEMRL |
| Manufacturing technology for polymers viz. t-GAP, Epoxy terminated Butadiene Isoprene Butadiene (BIB) and anionic Hydroxy Terminated Polybutadiene (HTPB) | HEMRL |
| Nitramine Grinding and spheridisation Plant for achieving reduced sensitivity and size reduction methods for Nitrmanes | HEMRL/ACEM |
| Pilot plant scale process for Raw & Prilled ADN | HEMRL |
| Pilot scale preparation of nano Boron, nanoAluminium, and nano metal oxides for HEM application using RF Induction Thermal Plasma Reactor | HEMRL |
| Propellant and igniters Composition and Processing | HEMRL |
| Propellant with greater Isp | HEMRL |
| Solid Propellant Self-extinguishment and Re-ignitable Propellant for Thrust Termination and Multi-pulse application | ASL |
| Solid Propulsion | Burn Rate Augmentation Prediction Model development | ASL |
| Semi-empirical 3D modeling of unsteady combustion response | DRDL |
| Solid Propellant Combustion Prediction Code Development | ASL |
| Solid Propulsion Performance Prediction code development | ASL |
| Virtual Six Component Testing of Rocket Motor - Software Model Development | DRDL |
| Automated Fibre Placement and Automated Tape Laying | DRDL |
| Casting Chamber for casting large rocket motors under vacuum level of 3 torr | HEMRL/ACEM |
| Casting of Multiple Large Solid Rocket Motors | ASL |
| Curing Oven for Rocket motor curing process | HEMRL/ACEM |
| Design and Realization technology for Composites | DRDL |
| Design and Realization technology for Nozzle Liners | DRDL |
| Hopper for propellant slurry with Electro-pneumatic discharge valve for slurry discharge into motor cast | HEMRL/ACEM |
| Hot Gas Valve based Solid Rocket Motors | ASL |
| Long duration solid propellant rocket motor | DRDL |
| Manufacturing technology for Composite Rocket Motor Casings (CRMCs) using Collapsible metallic fully reusable mandrel | DRDL |
| Motor Assembly Platform & Motor tilting fixture/Manual Tilter | HEMRL/ACEM |
| Out of Autoclave processing of Divergent Liners for Nozzles | DRDL |
| Special Purpose Machining technology for HD1.1 Propellant | HEMRL/ACEM |
| Three pulse motor technology with metallic barrier for Solid propulsion system | DRDL |
| Thrust Termination System for Upper Stage Rocket Motors | ASL |
| Granular or Flake Propellant for High Mach Muzzle Power Travelling Charge System Gun | ARDE |
| Multiple measurement techniques of propellant combustion response over wide frequency range at different initial temperatures | DRDL |
| Starter Generator | More Electric Propulsion with the gas turbine engine as the principal power-plant | GTRE |
| Sustainer | Boron Based Sustainer for Long Range Air to Air Missiles | DRDL |
| Hybrid Propulsion | Hybrid systems (Series/Parallel) for aero and ground applications including IC Engine, Motor, or Hydrogen Fuel cell, Motor | VRDE |
| Electric Propulsion | Scheme for In-situ Energy-Harvesting by AUVs during mission to avoid limitations imposed by battery charging requirements | NSTL |
| Electric Propulsion | Underwater Non-Contact Power Transmission and Reception | NSTL |
| Electric Propulsion | High Energy Batteries for fitment into man-portable AUV & XL-AUV | NSTL |
| IC Engine | Hydrogen based IC engines for aero and ground applications | VRDE |
| Propeller | Optimized Contra-Rotating highly Skewed Propeller Design for marine vessel applications | NSTL |
| Wankel Rotary Engine | Twin rotor Wankel type rotary engine for aero-application | VRDE |
