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.

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®

Aircraft range calculator

Explore payload, fuel and flight settings. Conceptual estimates only; not operational flight-planning data.

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