Discovery OS
Connect hypotheses, simulation workflows and experiment records. Agent proposals remain separate from human approval and execution authority.
VIMANA-X · Aerospace & Discovery
A new perspective on personal flight.
Aircraft design, advanced propulsion research and AI-native engineering. Connected by one ambition: better flight, built on stronger evidence.
HD Study · E0
VIMANA DUO/Two-seat companion study
High-definition study·Concept E0
Configuration
Annular Airframe
Bladeless rear ring
Propulsion
Resonant EAD
Solid-state physics
Acoustic Target
<45 dBATarget · E0Target. Evidence level E0: Claim only. Design target: under 45 dBA at 50 m for a solid-state propulsion platform.
At 50 m distance
Governance
Level E0 Study
VXM-RSC-EVD policy
Aircraft design explorer
AI-assisted design visualization · E0. Ring illumination is artistic.
Study the structural load paths, aerodynamic geometry and packaging interfaces before selecting a build configuration.
1 seat / Concept configuration
Single-seat personal aircraft
A slender single-seat aircraft study with a crystal canopy, swept stabilizers and a compact annular tail. Its long fuselage explores pilot access, controls and power-system packaging within a distinct personal-aircraft silhouette.
Next development gate
Structure and cockpit packaging study
01Research architecture
A connected loop between models and measurements.
The proposed architecture brings research software, physical experiments and independent review into a common workflow.
Propulsion research
Explore ion-to-air momentum transfer, electrode geometry and power electronics. Calibrated experiments determine the next development step.
Digital twins
Develop coupled electrical, thermal, structural and aerodynamic models. Check their predictions against retained physical measurements.
Evidence chain
Link claims to methods, assumptions, data and review history. Independent authority governs consequential decisions.
Concept illustration · E0 · not to scale
Research architecture study. Instrumented validation establishes model fidelity and system performance.
Inspect the EHD test-cell studyInspect the engine concepts
Mercury vortex chamberConcept · E0
A toroidal containment study with a banded metal shell, copper coil packs, ceramic feedthroughs and a central service sleeve. A quarter-section reveals the illustrative inner flow passage.
Open full image (opens in a new tab)Architectural elements
- 01Banded pressure vesselSteel shell with raised bands, sized as a placeholder.
- 02Copper coil packWound packs spaced around the tube.
- 03Cutaway wall sectionShows wall thickness and the interior.
- 04Annular flow passageIllustrative geometry for a contained medium.
- 05Central sleeveService passage through the torus hole.
- 06Bus ductPower and sensing feed-through.
Evidence boundary · E0
- No thrust, mass reduction or gravitational effect is established.
- The passage and cyan highlights are illustrative, not flow measurements.
- Containment and handling of mercury is an open engineering question.
Concept drawingIllustrative · E0Illustrative. Evidence level E0: Claim only. A toroidal vessel wound with copper coil packs is drawn as a concept for a closed-loop mercury vortex chamber.
Interior and interface architecture
01
A clear view
Panoramic crystal glazing and a quiet display hierarchy explore how the cabin could keep the outside world in focus.
02
Intelligence that explains
Proposed AI assistance connects system state, route context and recommendations with visible sources and uncertainty.
03
Human command authority
Tactile controls and an independent safety path remain part of the architecture. Assistance does not grant its own authority.
Concept illustration · E0 · not to scale
Interior and interface concepts · E0. Glazing, ergonomics, software behavior and safety architecture require engineering validation.
05Interactive concept theater
See the architecture from a different angle.
Inspect the aircraft concept as a render with stylized airflow, or turn a 3D wireframe of the annular airframe to see how the ring, pod and electrode array fit together.
Aircraft design study · E0
Concept render / illustrated airflowView pitch 0° · View yaw 0°
-15 °15 °
-20 °20 °
Airflow lines are illustrative. This viewer does not calculate aerodynamic forces or represent flight-test data. Animation respects reduced-motion preferences.
Compare the sources of sound.
These synthetic frequency shapes illustrate a research question. They are not measured spectra or sound-level predictions.
Solid-state EHD
Primary source / Ion-driven airflow
Concept illustration · E0 · not to scale
EHD avoids blade-passage noise. Discharge, power electronics and airflow still require acoustic characterization. VIMANA-X has no measured full-vehicle acoustic result.
Confidence is earned at every level.
A public claim follows the maturity of its evidence. Aircraft and engine artwork on this site remains a concept at E0.
Research records retain methods, data, corrections and review decisions. Requesters cannot approve their own requests. Models propose work; authorized humans approve consequential decisions.
- E0
Claim only
An idea or concept, without supporting analysis or measurement.
- E1
Theoretical support
A theoretical basis with defined assumptions and bounds.
- E2
Simulation
A model run with retained inputs, methods and uncertainty.
- E3
Single experiment
A calibrated measurement with methods and source data.
- E4
Repeated internally
Repeated results within the originating research team.
- E5
Independent replication
Reproduction by an independent team with inspectable methods.
- E6
Vehicle or system validation
Integrated performance demonstrated at system level.
- E7
Operational validation
Performance validated within a defined operational envelope.
Published research baseline / external work
Electroaerodynamic fixed-wing flight.
Repeated flights reported by the original teamCited result · E4Cited result. Evidence level E4: Repeated internally. A 5 m-class fixed-wing aircraft completed ten powered electroaerodynamic flights. Register: EXP-EAD-001.
Xu and colleagues reported ten powered flights of a five-metre fixed-wing aircraft in 2018. This is an external research baseline. It establishes neither passenger VTOL performance nor independent replication by VIMANA-X.
Read the Nature paper (opens in a new tab)Our concept studiesVXM-RSC-EVD-001 · public claims cannot exceed their evidence
03 / Investor & partner perspective
Build value at every stage.
Research infrastructure and specialized systems create a potential commercial path before passenger aircraft. Development advances through explicit evidence gates.
Strategy & development roadmap04Design & research insights
The thinking behind the concepts.
Read the architecture, assumptions and validation questions behind the studies.
Propulsion concepts
Inside the electromagnetic architecture study
Explore the coil, resonator stack and cavity as a packaging concept, together with the measurements needed to evaluate it.
Read the studyHardware studies
The mercury chamber: design begins with containment
A sectioned vessel makes the proposed shell, coil packs, inner passage and service interfaces visible.
Read the studyCabin & interfaces
Crystal cockpit: intelligence with clear authority
Panoramic glazing, integrated displays and physical controls explore a cockpit centered on awareness and human command.
Read the study