TECHNICAL DATA / 03

Every measure of progress.

AERION 01 is being developed to combine high-speed electric cruise with the operational freedom of vertical takeoff and landing.

320KM/H

MAX CRUISE

480KM

PROJECTED RANGE

04EPU

PROPULSION UNITS

04SEATS

CABIN CAPACITY

01 — ENGINEERING ARCHIVE

SYSTEMS IN CONTEXT

Designed as one machine.

Airframe, propulsion, cabin and landing architecture are resolved together—each system informing the next.

AERION 01 engineering blueprint sheet showing the airframe, propulsion, cabin and landing systems — AERION ENGINEERING / ADVANCED eVTOLREFERENCE PLATE 01

PLATE 02 / STRUCTURAL MODEL

Surface intelligence.

A digital wireframe exposes the continuous load paths beneath the sculpted bodywork and the relationship between propulsion, canopy and stabilizing surfaces.

AERION 01 wireframe engineering study with propulsion, canopy, fuselage and stabilization callouts — COMPOSITE SURFACE MODELREFERENCE PLATE 02

Performance

Maximum cruise speed320 km/h199 mph

Projected range480 km298 mi

Service ceiling4,500 m14,764 ft

Hover noise at 100 m< 65 dBATarget

Architecture

Propulsion4 independent EPUElectric

Energy storageStructural batteryLiquid conditioned

AirframeCarbon compositeMonocoque

Flight controlTriplex digitalEnvelope protected

Dimensions

Overall length6.42 m21.1 ft

Overall width7.10 m23.3 ft

Height2.18 m7.2 ft

Cabin capacity4 occupantsIncluding pilot

Ownership

ChargingDC rapid charge20–80% target

Digital support24 / 7Concierge

ConfigurationBespokeBy commission

ProductionLimited seriesPriority allocation

All specifications are design targets and may change during development, certification and production engineering. Range and performance vary with payload, atmospheric conditions and mission profile.

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