Overview

Kesari develops UAV platforms as complete aircraft: the configuration, aerodynamics, structure and propulsion installation are engineered together against a defined mission, rather than assembled from a fixed airframe.

We take a mission requirement — speed, altitude, range, endurance, payload, launch and recovery, operating environment and signature — and translate it into aircraft-level design requirements before a configuration is selected.

What we support

Complete UAV development programmes, and the early conceptual and preliminary-design phases that de-risk a programme before detailed design begins.

Engineering scope

Mission requirements definition and interpretation
Conceptual design
Configuration development
Preliminary sizing
Aerodynamic layout
Wing loading & thrust loading
Mass and CG development
Aircraft-level trade studies
Propulsion matching
Design baseline definition

Typical inputs

Mission and operating requirements
Payload and sensor constraints
Launch / recovery method
Environmental and range requirements
Programme and manufacturing constraints

Typical deliverables

Aircraft-level requirements set
Configuration baseline and layout
Preliminary mass / CG and loading budgets
Aerodynamic and performance summary
Development roadmap to detailed design

Where it fits in aircraft development

This is the front of the aircraft-development process: it produces the configuration baseline that aerodynamics, structures, stability & control and propulsion integration all build on, and it feeds directly into the stage-gated development flow through to flight test.

Why Kesari

Kesari leads at aircraft-level — configuration, requirements and integration — combining contemporary UAV engineering and digital methods with senior aircraft-design experience across fighter, trainer and unmanned aircraft programmes.

UAV Design & Development