Airframer
Programs › Joby S4

Aircraft program

Joby S4

In production
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1 pilot + 4 passenger eVTOL with 6 propellers that transition to forward flight, capable of a maximum cruise speed of 200 mph. Includes variant S2 with 12 propellers, and technology demonstrator / pre-production models Joby S4 Generaton 1.0 / 2.0 respectively.

Lift type
Tilt-rotor
Assembly
Factory-built
Control
Piloted
Engine type
Electric
Application
Experimental, Urban air mobility

Design & construction

The aircraft as engineered: what it is built from, the systems it flies with, and its configuration — each box a theme.

Airframe & structure
Primary structure
Composite
Wing
Composite
Landing gear
Retractable tricycle
Ice protection
None
Pressurisation
Unpressurised
Systems & avionics
Flight controls
Full FBW digital
Autopilot
3-axis
Avionics architecture
Integrated glass suite
Configuration & certification
Minimum crew
1

Notable technologies — each tag names a technology on our research record for this aircraft, with its fitting status: Primary, Standard, Option or Planned.

Synthetic vision Standard

Technical reference compiled with AI research; a value appears only where two independent research passes and a web fact-check agree. Gaps are deliberate.

A deeper insight into the Joby S4

Supplier geography and market analysis for this program — with an Analytics subscription.

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The industry ledger — an Analytics feature — holds every dated event on this program: contracts, certifications, first flights and appointments, each linked to its source. See a worked example →

Type variants

VariantLaunch / first flightProduction endNotes
Joby S22014 / 2015Two-seater eVTOL with 12 propellers, development ceased in favour of S4.
Joby S42015 / 2017Five-seater tilt-rotor eVTOL.
Joby JAI 302025 / 2025Hydrogen-electric unmanned development with SuperPilot autonomy. Also referred to as turbine electric, autonomous VTOL demonstrator or S4-T.

Airframer

Joby Aviation, Inc.News

The program’s dated history — milestones, contracts, supplier selections and facilities, each linked to its source. Log in to view.

Information on this page is compiled from a variety of published sources; links do not necessarily imply recommendation or confirmation by the airframe manufacturer.

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