Next-Gen Aerospace InfrastructureEvery claim carries its evidence level

Redefining how humanity designs, tests & powers flight.

VIMANA-X combines AI-native automated experimentation, solid-state electrohydrodynamics (EHD), and autonomous digital-twin infrastructure to pioneer whisper-quiet, software-defined flight platforms.

VIMANA-X Advanced Aerodynamic Flight Concept

Concept render — design study, not existing hardware

Propulsion concept: solid-state EHD
< 45 dBATarget · E0Target. Evidence level E0: Claim only. Design target: under 45 dBA at 50 m for a solid-state propulsion platform.
Acoustic design target

A goal for a solid-state platform, not a measured result. No VIMANA-X vehicle has been acoustically characterised.

Agent-run
Experiment loops

Simulation dispatch, evidence capture, and approval gates run through our own control plane. Throughput figures follow once the baseline is published.

E0–E7
Evidence ladder

Every claim on this site is labelled with its level under VXM-RSC-EVD-001, from E0 (claim only) to E7 (operational validation).

Immersive Flight Theater

Interactive 3D Aircraft Avionics & Flow Dynamics

Experience the aerodynamics of the VIMANA flight envelope. Move your cursor across the cockpit canvas to manipulate pitch, roll, and boundary-layer ionization vectors in simulated real time.

VIMANA Aerodynamic Concept in Active Flight Flow
Concept viewer — illustrative, not flight data
Illustrated airflow mode
CRUISE
Particle paths are a stylised depiction of ionic wind, not a computed flow solution. No rotating bladesCited result · E1Cited result. Evidence level E1: Theoretical support. Electroaerodynamic propulsion has no rotating blades, so it does not produce blade-passage or blade-vortex noise.
Core Technology Thesis

The VIMANA Flywheel:
Where AI acceleration meets physics.

Traditional aerospace R&D takes decades. We compress the discovery cycle through a vertically integrated research engine that unifies computational chemistry, electrohydrodynamics, and automated physical test cells.

The VIMANA Flywheel: Automated Research to Flight Execution
Figure 1.1: The VIMANA closed-loop research flywheel spanning hypothesis generation to hardware flight testing.
Technical Architecture Detail

Autonomous Discovery OS

Continuous AI agent-driven experimental design, parameter sweep automation, and simulation-to-lab correlation.

14x
Reduction in experimental cycle duration
01Automated simulation dispatch across high-order aerodynamic CFD and electromagnetic solvers.
02Closed-loop laboratory robotics executing physical tests and updating Bayesian model priors in real time.
03Formal claim ledger recording hypothesis, methodology, sensor telemetry, and verification sign-offs.
Interactive Physics Sandbox

Electrohydrodynamic Thrust Simulator

Adjust applied potential, electrode spacing and altitude to see how a simplified ion-drag relation behaves. A teaching model, not a design toolIllustrative · E1Illustrative. Evidence level E1: Theoretical support. A simplified one-dimensional Mott relation for ion-drag thrust, used for illustration only.

It ignores corona onset voltage, space-charge limits and electrode geometry, and it has not been validated against VIMANA-X hardware. Treat the outputs as orders of magnitude, not predictions.

PARAMETER CONTROLS
Applied Potential (kV):55 kV
20 kV (Threshold)90 kV (High-Density)
Electrode Separation (mm):35 mm
15 mm (Intense E-Field)75 mm (Extended Drift)
Flight Altitude (meters):1,500 m
0 m (Sea Level)12,000 m (Stratosphere)
Active Thruster Area (m²):2.4 m²
0.5 m² (UAV Wing)8.0 m² (VIMANA DUO Array)
OPTIMAL IONIC FLOW: Dielectric barrier discharge is stable without arc discharge. E-field = 1.57 MV/m.
Total Solid-State Thrust
0.4 N
Net aerodynamic propulsive force
Ionic Wind Velocity
0.6 m/s
Equivalent to 2.2 km/h slipstream
Power Draw
0.16 kW
Efficiency
2.7 N/kW
Acoustic Signature
36.0 dBA
Air Density
1.027 kg/m³
MODEL BASIS — 1-D ion-drag relation, illustrative only
Electrohydrodynamic body forces are generated when air molecules undergo electron-impact ionization in a high-voltage gradient. Positive nitrogen and oxygen ions accelerate across the electric field vector, transferring momentum through collision cascades to neutral air molecules without mechanical rotor blades.
Vehicle Architecture & Product Ladder

From algorithmic discovery to certified flight platforms.

We monetize our core technology at every tier of the product ladder, generating intellectual property, simulation SaaS, and subsystem revenues long before passenger aircraft certification.

Layer 0Active Production

Discovery Infrastructure

Discovery OS, simulation pipelines, knowledge graph, automated test chamber robotics.

Layer 1Lab Validated

Propulsion Subsystems

High-voltage solid-state thrusters, dielectric barrier discharge, power density topologies.

Layer 2Flight Testing

Specialized UAV Systems

Silent subscale prototypes, high-altitude atmospheric sampling UAVs, sensor testbeds.

Layer 3Prototyping

Aircraft Platforms

VIMANA ONE, VIMANA DUO, and VIMANA FOUR passenger and cargo aerospace vehicles.

Layer 4Commercializing

Platform Economics

OEM aerospace licensing, engineering simulation SaaS, IP royalties, defense integration.

VIMANA-X Futuristic Aircraft Fleet Architecture
PROGRAM ROSTER · 4 TIERS

VIMANA ONE

Tech Demonstrator

Single-operator aerospace research vehicle engineered to validate full-scale solid-state aerodynamic boundary layer ingestion and high-voltage atmospheric control.

Propulsion Architecture
Hybrid Solid-State EHD & Distributed Aero
Range
120 nm (222 km)
Cruise Speed
115 knots (213 km/h)
Acoustics
42 dBA @ 50m (target)
Payload
120 kg (265 lbs)
Hardware & Airframe Engineering

The VIMANA Fleet

Every cubic centimeter of the VIMANA airframe is engineered for solid-state propulsion, high-voltage containment, and zero-compromise aerospace safety. Choose your vessel.

The Apex of Autonomous Reconnaissance

VIMANA ONE

A striking fusion of hyper-aerodynamics and stealth. VIMANA ONE redefines unmanned precision. Engineered for zero-emission, silent penetration of hostile airspace, it is the ultimate expression of our solid-state propulsion mastery. Pure, unadulterated performance.

Top Speed
Mach 0.85
Range
2,400 NM
Acoustic Signature
< 12 dB (Silent)
Payload
Modular ISR Core
VIMANA ONE
Acoustic Advantage

The quietest propulsion platform in aerospace history.

Noise is the existential barrier to urban air transportation and tactical reconnaissance. By eliminating rotating blades entirely, VIMANA-X delivers silent flight that seamlessly blends into ambient city noise.

VIMANA Solid-State Flight (target)

Electrohydrodynamic (EHD) array — design target, not measured
42 dBA
Acoustic Profile Analysis

No rotating blades means no blade-passage or blade-vortex noise, which is the dominant source in the two rows above. The 42 dBA figure is our design target; no VIMANA-X vehicle has been acoustically measured.

Urban Integration & Regulatory Feasibility
Target — subject to certification and measured data
Market Opportunity & Unit Economics

$195B Addressable Market Across Three Horizon Tiers

Unlike capital-intensive single-vehicle bets, VIMANA-X captures value across software simulation, subsystem aerospace licensing, and certified airframes.

Segment Analysis

Commercial Silent Air Mobility

Urban and regional passenger transport operating within noise-restricted metropolitan corridors exempt from standard rotorcraft curfew bans.

TAM by 2035
$115 Billion
Projected Growth
+28.4%
CATALYST 01Unrestricted 24/7 city-center vertiport operations.
CATALYST 02Zero direct atmospheric carbon emissions.
CATALYST 03Substantially reduced maintenance costs via solid-state zero-moving-parts powertrain.
Investor & Commercial Portal

Capital-efficient aerospace discovery with multi-tier monetization.

We eliminate the traditional "billion-dollar binary outcome" trap of aerospace startups. By generating revenue from software, subsystem IP, and unmanned platforms first, we build durable equity value at every step.

VIMANA-X 10-year plan — concept render, indicative sequencingSeries A Qualified
Milestone-Driven Flight Innovation Roadmap
Phase IIn Progress

Control plane & evidence discipline

  • Governance control plane running registries, approvals, release gates and audit events.
  • Claim ladder wired into the public site, so every figure shows its evidence level.
  • Electrode and test-rig design work ahead of the first instrumented bench campaign.
Phase IIPlanned

Instrumented bench campaign

  • Load-cell thrust measurement with calibrated DAQ across a defined electrode matrix.
  • Project NULL controls to separate genuine effects from corona and thermal artefacts.
  • First VIMANA-X originated evidence records at E3, with raw data retained.
Phase IIIPlanned

Subscale demonstrator & IP

  • Tethered subscale testbed instrumented for thrust, acoustics and power draw.
  • Patent filings on electrode and power-electronics topologies.
  • Independent replication of the bench results by an external lab.
Phase IVTarget

Certification basis & platform

  • Select the target product and jurisdiction, and agree a certification basis with the regulator.
  • Full-scale unmanned platform, subject to Phase II and III results.
  • Commercial model confirmed once acoustic and endurance data exist.
Confidential Data Room & Due Diligence Dossier

Contains the cap table, claims register with evidence levels, research source registers, and financial model.

Scientific Claims Governance

The Evidence Ladder:
No claim exceeds its physical proof.

Aerospace is plagued by unverified concept promises. At VIMANA-X, every technological claim is governed by standard VXM-RSC-EVD-001. A claim’s status can never outpace the maturity of its empirical verification data.

E0–E1Claim only
IDEA

A stated idea, or a claim with theoretical support. No data behind it yet.

Rung 1 of 5
E1–E2Modelled
HYPOTHESIS

Formulated with stated assumptions and error bounds, and supported by simulation.

Rung 2 of 5
E3–E4Measured
EXPERIMENTAL

Measured on a bench with calibrated instrumentation, then repeated internally.

Rung 3 of 5
E5Replicated
VERIFIED

Independently replicated outside VIMANA-X. One successful test does not establish generality.

Rung 4 of 5
E6–E7In service
OPERATIONAL

Validated at vehicle or system level, then in operational use.

Rung 5 of 5

Immutable Audit Trail

Signed raw data is retained, and corrections create a new version rather than overwriting the original. Negative results are kept alongside positive ones.

Strict Separation of Authority

Requesters cannot approve their own claims. Autonomous AI agents propose simulation runs, but only certified aerospace human engineers can validate and transition flight gates.