Skip to content
eos-aero · Concept Design

Solar-Hybrid VTOL Aircraft

AeroSwift is a concept family of solar-hybrid vertical-takeoff aircraft and a research software architecture. No aircraft has been flight-tested or certified.

2
Concept Designs
480 kWh
Battery Target
VTOL
Design Goal
AeroOS
Research OS

Two Vehicle Concepts

Illustrative 3D concept renders with simulated telemetry. Values shown are design targets pending hardware and flight testing.

Concept 3D Render
VTOL
Simulated Flight Telemetry● SIMULATED
1–2
Target Capacity
90 kWh
Target Battery
300+ km
Target Range

AeroSwift-Personal (AS-1/2)

Personal Air Vehicle Concept

Concept design for a 1-to-2 passenger personal air vehicle. Foldable wings, solar-hybrid propulsion, a 90 kWh battery, and 300+ km range are design targets, not flight-tested specifications.

Design Feature
Foldable Wings
Target Speed
185 mph
Target Altitude
1,200 ft
Target use: consumer commuteDesign goal: garage storageProposed autonomous flight modesProposed touchscreen controls
Concept 3D Render
VTOL
Simulated Flight Telemetry● SIMULATED
10
Target Capacity
480 kWh
Target Battery
320 km
Target Range

AeroSwift-Transit (AS-10)

Urban Air Taxi Concept

Concept design for a 10-passenger urban-air-mobility shuttle. Cabin capacity, a 480 kWh solid-state battery, redundancy, and performance figures are design targets, not flight-tested specifications.

Design Target
Triple-Redundant
Target Speed
210 mph
Target Altitude
2,800 ft
Target use: commercial air taxiProposed wide-body cabinPlanned fleet managementAeroOS research architecture

AeroOS Technology Stack

A research architecture targeting aerospace safety objectives. It has not been certified for safety-critical flight.

AeroOS
Research operating-system design for flight-control studies
Flight Computer
Proposed 8-layer and 12-layer TMR PCB designs
Solar-Hybrid Drive
Proposed photovoltaic and battery propulsion concept
BLE + 5G Telemetry
Planned fleet telemetry and control research
Solid-State Battery
480 kWh energy-storage design target
VTOL Aerodynamics
Proposed vertical-takeoff-and-landing architecture

Open Aerospace Research

Explore the available research designs and software, contribute evidence, or use the concepts as a starting point for independently validated aerospace work.