UAV Design & Platform Engineering · India

From mission requirements to flight‑ready UAV platforms.

Aircraft configurationAerodynamicsStructuresPropulsionFlight validation

Aircraft-Level Engineering Digital Development Concept → Flight Test

Kesari development programmes

Our UAV development spectrum.

KAT-LS1 low-speed aerial target — isometric CAD view

KAT-LS1

Low-speed aerial target · counter-UAS training

MTOW
30 kg*
Speed
200 km/h*
Variants
1E / 1R
Amogha high-speed jet UAV concept render

Amogha

Single-jet high-speed UAV

MTOW
90 kg*
Speed
400 km/h*
Range
400 km*
Schematic

Amogha Mk2

Twin-jet high-speed UAV

MTOW
140 kg*
Speed
700 km/h*
Range
800 km*
KAS-M1 transonic low-observable UAV concept render Flagship

KAS-M1

Transonic low-observable UAV

Speed
Mach 1*
Propulsion
Turbojet*
Airframe
Low-obs.*

* Preliminary design targets under active development — not flight-demonstrated, not necessarily simultaneous, and subject to detailed engineering and flight validation. No measured RCS or demonstrated Mach number is claimed for KAS-M1.

Aircraft development

The mission defines the aircraft.

SpeedRangePayloadAltitudeEnduranceSignature
Mission requirements → Requirements baseline

Configuration. Sizing, trade studies, mass/CG, wing and thrust loading, and the aircraft architecture every later discipline works from.

Aerodynamics. Lift, drag and moment prediction, aerodynamic databases, control studies and compressible-flow CFD.

Performance. Flight envelope, range, endurance, climb, ceiling and propulsion matching across the mission profile.

Stability & control. Static and dynamic stability, neutral point and static margin, control-surface sizing and effectiveness.

Structures. Loads, metallic and composite sizing, FEA, stiffness, modal analysis and weight optimisation.

Propulsion. Engine–airframe integration, inlet/exhaust installation, fuel-system interfaces and installed performance.

Manufacturing. Production-intent design, tooling definition, assembly strategy, drawings and inspection requirements.

Flight test. Ground-test readiness, instrumentation, test cards, flight-data reduction and aerodynamic correlation.

Platform integration

Kesari leads the aircraft platform.

Aircraft platformKesari
  • Airframe
  • Aerodynamics
  • Structures
  • Performance
  • Propulsion
  • Flight Test
Aircraft-level interfaces
  • Avionics
  • Electrical
  • Embedded / FCC

Specialist partners

Kesari establishes the aircraft configuration, requirements and interfaces on Kesari-led programmes; specialist systems integrate against that baseline.

On customer programmes, Kesari works within the customer's Design Authority.

Development process

Stage-gated aircraft development.

  1. Mission
  2. Requirements
  3. SRR
  4. Concept
  5. PDR
  6. Detail Design
  7. Verification
  8. CDR
  9. Manufacture
  10. Ground Test
  11. Flight Test
  12. Design Closure
Engineering stageReview gateSRR · System Requirements Review   PDR · Preliminary Design Review   CDR · Critical Design Review

Simulation informs design decisions and reduces risk; it does not replace ground and flight testing.

About Kesari

Indian aerospace engineering & UAV development.

Kesari Aerial Systems Pvt. Ltd. focuses on aircraft configuration, airframe development and aircraft-level integration.

40+ yrs
Senior aircraft-design experience (advisory)
Concept → Flight
Aircraft development capability
New Delhi
India

Supported by a retired HAL Chief Designer serving as Technical Advisor.

Our vision

To build Kesari Aerial Systems into a leading aircraft design and airframe development company, specialising in advanced UAV platforms, high-speed flight and low-observable technologies.

Contact · technical discussion

Discuss an engineering programme with our team.

Start with a short technical brief.

LocationNew Delhi, India
ResponseWe aim to respond within 24 hours

Confidential technical discussions can be conducted under NDA.

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