Jetoptera aims to be the platform powering the future of air mobility

Five aircraft. One Adaptive Fluidic Propulsive System®.

The J-Series applies Jetoptera's bladeless propulsion architecture across cargo, agricultural and passenger aircraft concepts. Each platform is designed around its mission while sharing a focus on vertical or short-field access, efficient forward flight and a tone-free noise profile up to 40 dBA lower than a bladed equivalent power system.

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Product lineup

The J-Series

Select an aircraft for key details, mission uses and its downloadable August 2026 specification sheet.

Delivery targets are estimates and remain subject to regulatory approval and development milestones. Aircraft shown are concepts and prototypes in development.

Cargo UAS | Proposed FAA Part 108 pathway

J-110 "Pegasus"

Target first delivery2027
J-110 Pegasus cargo aircraft concept in flight

Concept aircraft shown. Configuration and specifications may change.

Max payload55 lb
Max range240 mi
Cruise speed100 mph
Max speed150 mph

The J-110 is a bladeless VTOL cargo concept designed for rapid logistics and access to constrained locations. Its Adaptive FPS® architecture eliminates exposed propellers and rotors while targeting a lower, atonal noise profile.

Designed for

  • Last-mile cargo delivery
  • Pipeline and infrastructure inspection
  • Public safety and emergency response
  • Defense and military missions

Configuration

Fuel
Jet A / Diesel
Max takeoff weight
110 lb (50 kg)
Propulsion
4 Adaptive FPS® thrusters, 40 lbf class
Dimensions
12.5 x 14.7 x 4.4 ft
Agricultural VTOL UAS | Proposed FAA Part 108 pathway

J-600 AG

Target first delivery2027
J-600 AG agricultural aircraft concept operating over a field

Concept aircraft shown. Configuration and specifications may change.

Max payload400 lb
Ferry range*400 mi
Hopper capacity50 gal
Coverage / load16 acres

The J-600 AG combines high-capacity agricultural utility with true vertical takeoff and landing. It is designed to operate from field edges and constrained sites while supporting faster transit between fields than a conventional multirotor.

Designed for

  • Crop spraying and fertilizer application
  • Seeding and field mapping
  • Multispectral and continuous field monitoring
  • Livestock and pasture monitoring

Configuration

Fuel
Jet A / Diesel
Max takeoff weight
600 lb (272 kg)
Speed
100 mph Part 108 cruise; 150 mph max
Propulsion
75 lbf class FPS® + cruise nozzle
Agricultural STOVL UAS | Proposed FAA Part 108 pathway

J-900 AG STOVL

Target first delivery2027
J-900 AG STOVL agricultural aircraft concept operating over a field

Concept aircraft shown. Configuration and specifications may change.

Max payload700 lb
Ferry range*800 mi
Hopper capacity85 gal
Coverage / load28 acres

The J-900 AG STOVL combines Adaptive FPS® with an upper-surface-blown-wing architecture for short takeoff and vertical landing. The concept targets takeoff in less than 100 feet with a large load, followed by a vertical landing after the hopper is empty.

Designed for

  • High-capacity crop spraying
  • Fertilizer application and seeding
  • Field mapping and multispectral monitoring
  • Livestock and pasture monitoring

Configuration

Fuel
Jet A / Diesel
Max takeoff weight
900 lb (408 kg)
Speed
100 mph Part 108 limit
Propulsion
FPS® + upper-surface-blown-wing nozzles
Two-seat passenger VTOL | FAA MOSAIC / Special-LSA pathway

J-2000

Target first delivery2028
J-2000 two-seat passenger aircraft concept in vertical flight

Concept aircraft shown. Configuration and specifications may change.

Max payload500 lb
Max range400 mi
Cruise speed150 kn
Max speed200 kn

The J-2000 is the introductory two-seat passenger platform in the J-Series. Its box-wing and canard architecture is paired with swiveling FPS® thrusters to combine vertical access with efficient forward flight.

Designed for

  • Personal and family travel
  • Recreation and hobby flying
  • Flight training
  • Two-seat point-to-point mobility

Configuration

Cabin
Pilot + 1 passenger
Fuel
Jet A / SAF
Max altitude
10,000 ft MOSAIC limit
Propulsion
2 x 250 + 2 x 1,000 lbf FPS®
Four-seat passenger VTOL | FAA MOSAIC / Special-LSA pathway

J-4000

Target first delivery2029
J-4000 four-seat passenger aircraft concept over Seattle

Concept aircraft shown. Configuration and specifications may change.

Max payload1,000 lb
Max range400 mi
Cruise speed150 kn
Max speed200 kn

The J-4000 extends the J-Series passenger concept to a four-seat cabin. It is designed around the same no-exposed-rotor architecture, efficient box-wing configuration and vertical flight capability as the smaller J-2000.

Designed for

  • Personal, family and group travel
  • Recreation and hobby flying
  • Flight training
  • Four-seat point-to-point mobility

Configuration

Cabin
Pilot + 3 passengers
Fuel
Jet A / SAF
Max altitude
10,000 ft MOSAIC limit
Propulsion
2 x 750 + 2 x 2,000 lbf FPS®