Research you can see, touch and drive.
Simulation and analysis for DRDO laboratories, vehicle and defence engineering with industry, and indigenous test facilities built for the Indian Air Force and Indian Navy.
33 projects

Tri-Sonic Wind Tunnel
A wind tunnel spanning subsonic, transonic and supersonic regimes — Mach 0.4 to 4 across 30–40 second runs for aerospace-vehicle testing.

UV Disinfectant Bot
An autonomous robot that sanitises workspaces with UV-C light — built during the COVID-19 pandemic to keep shared spaces infection-free.

Reverse Engineering of a Seeker Head Gimbal System
Full reverse engineering of a seeker head gimbal — kinematics, metrology, 3D models and manufacturing drawings for indigenous manufacture.

Development Study of Copper Tulip Liner
Process plan development for a sheet-metal forming route, established through non-linear finite element analysis.

Thermal & Structural Simulation of an ESM RF LRU Assembly
CFD study of heat dissipation and cooling-fan selection for an RF line-replaceable unit, paired with FEA for structural integrity.

Design & Analysis of a Passenger Access Ladder
A variable-height access ladder taken from concept to fabrication — 3D design, structural verification and manufacturing support.

FEA of a Paddy Soaking Tank
Strength and stability verification of an industrial soaking tank across its filling, soaking and discharge cycle.

CFD Analysis of Flow over and within an Active Antenna Array Unit
Internal and external CFD simulations of airflow around an aircraft-mounted Active Antenna Array Unit.

Engine Installation & Cooling Flow Study on a MALE UAV
Combined internal and external CFD study of cooling requirements and installation losses for a medium-altitude long-endurance UAV.

Performance Improvement of a Micro Propulsion System for UAVs
Design modifications to the turbine and nozzle of a micro gas turbine to raise overall propulsion performance.

BLDC Motor & Fuel Pump Design Validation for the ALH
Design and validation of a BLDC motor for the fuel pump used in the Advanced Light Helicopter, verified by CFD and FEA.

Structural Analysis of a Hydraulic Press
FEA-based assessment of a hydraulic press carrying very high compressive loads, to establish design safety and improvements.

Reliability Analysis of AEW&C Primary and Secondary Surveillance Radar
Component-level reliability prediction for the line-replaceable units of an airborne early warning and control radar installation.

CFD Analysis of Backflow in a Twin-Screw Pump
Simulation of leakage flow through the internal clearances of a twin-screw pump across its operating range.

Numerical Analysis of a Tri-Sonic Wind Tunnel Nozzle System
Design of a variable Mach number nozzle system spanning subsonic, transonic and supersonic operation, developed through theory and CFD.

Loading Life-Cycle Study of Missile Lugs, Bolts and Inserts
Life-cycle limitation study of the removable lugs and fasteners that secure a store to the fixed wing of a maritime surveillance aircraft.

Tractor Electrification — Powertrain Integration
A diesel tractor converted to a reliable electric machine for industrial use — powertrain mounts designed, integrated, validated and tested.

Autonomous Campus Utility Vehicle
A driverless campus utility vehicle supporting manual, remote and autonomous modes, built around AI perception, RTK GPS and CAN communication.

All-Wheel Drive & Steering Unmanned Ground Vehicle
An unmanned ground vehicle with drive and steering on every wheel, developed for demanding off-road and defence duties.

Main Rotor Lead-Lag Damper for Helicopters
Indigenous design and development of the main rotor lead-lag damper used on ALH and LUH helicopters, for rotor stability on the ground and in flight.

Test Rig for an Injection Timing Device
A purpose-built rig for exercising and verifying the operation of an engine injection timing device.

Wing Opening and Locking Mechanism
A torsion-spring wing deployment mechanism with a mechanical stopper for secure locking, taken from design through prototype and test.

UAV Launcher System
A UAV launcher developed and proven through repeated launch trials across a range of payload masses and inclinations.

Suspension, Axle Arm and Hub Assembly for a Tracked Vehicle
Design refinement of a tracked vehicle running-gear assembly, with sealing optimisation and a full manufacturing and acceptance package.

Shock Absorber for All-Terrain Vehicles
Reverse engineering and redesign of a hydro-pneumatic shock absorber, delivered as models and manufacturing drawings.

Tester for the IL-76/78 Engine Control Unit
The first tester of its kind developed in India for the engine control unit of the IL-76/78 heavy lift aircraft — six units supplied.

Tester for the Aircraft Fatigue Meter
Refurbishment and development of a test set for the aircraft fatigue meter, restoring serviceability for an in-service system.

Repair of the Gun Control Unit of a Fighter Aircraft
Indigenous recovery of obsolete high-value fighter aircraft units — six restored, validated and returned to operational service.

Test Facility for an Aircraft ECS Evaporator Assembly
A facility that simulates the cockpit environment control system to exercise and verify the evaporator assembly.

Indigenous Test Facility for a Fighter Aircraft Intercom Control System
A ruggedised, mil-grade facility for testing air-to-air and air-to-ground communication equipment — transferred to the Air Force with documentation.

Test Facility for the Dornier Anticollision Lamp Power Controller
A facility that simulates and verifies the operation of the anticollision lamp power controller fitted to the Dornier.

Test Facility and Refurbishment — Ejection Seat Actuator Assembly
A laser-based, touch-screen test facility for the ejection seat actuator, paired with refurbishment technology that extends Air Force MRO capability.

Pressure Testing Kit for the Main Gearbox and Engine
Ground support equipment for checking the serviceability of the main gearbox and engine oil cooler, in a compact single kit.
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Research, consultancy, product development or a competency centre of your own — start a conversation with the KCIRI team.