Overview

Propulsion integration is where the powerplant becomes part of the aircraft. Kesari matches and installs propulsion so that installed performance, structure and thermal behaviour all work together.

Platform development and propulsion integration across electric, internal-combustion-engine and turbine-powered UAV architectures, selected according to mission, speed, altitude, endurance and payload requirements.

What we support

Propulsion selection, matching and installation for new platforms, and integration support for existing aircraft. Kesari integrates propulsion; it does not manufacture engines.

Engineering scope

Propulsion matching
Installed-performance assessment
Propulsion-airframe interaction
Inlet / exhaust installation considerations
Fuel-system interface requirements
Structural integration
Thermal integration
Electric / IC-engine / turbine architecture selection

Typical inputs

Mission and performance requirements
Candidate powerplant data
Configuration and volume constraints
Thermal and structural context

Typical deliverables

Propulsion selection and matching
Installed-performance assessment
Installation and interface definition
Structural / thermal integration requirements
Integration definition for detailed design

Where it fits in aircraft development

Propulsion integration draws on aerodynamics, structures and performance and produces the installation definition the airframe is built around — a central integration activity.

Why Kesari

Mission-first propulsion selection across electric, IC-engine and turbine architectures, integrated at aircraft level rather than bolted on.

Propulsion Integration