DarkAero 1
2 Occupants
Side by Side
1 2 3 4 5 6 7 8 9 0
1 2 3 4 5 6 7 8 9 0
0 1 2 3 4 5 6 7 8 9
mph
275 mph
Cruise Speed
1 2 3 4 5 6 7 8 9 0
1 2 3 4 5 6 7 8 9 0
0 1 2 3 4 5 6 7 8 9
0 1 2 3 4 5 6 7 8 9
sm
1700 sm
Range at 275 mph
750 lb
Useful Load
Every aircraft is designed for a mission, and our mission required speed, range, and efficiency. No aircraft had the right capabilities to meet our needs, so we set out to develop our own. We selected a lightweight but powerful engine and built an airframe around it using the strongest and lightest materials. The result of these efforts is the DarkAero 1.

DarkAero 1 Projected Specs


Cruise Speed
275 mph
Stall Speed
70 mph
Rate of Climb
2500 ft/min
Fuel Capacity
77 US gallons
Length
18 ft
G Loading
Normal Category
Landing Gear
Tricycle Retractable
Range at 275 mph
1700 sm
Useful Load
750 lb
Empty Weight
750 lb
Horsepower
200 hp
Wingspan
23 ft 5 in
Cockpit Width
43 in
Wing Area
66 ft2
Ceiling
20,000 ft





Engine

The airframe of the DarkAero 1 is designed specifically around the 200 hp, electronically controlled UL Power UL520iS engine. The UL520iS is significantly lighter and smaller than traditional aircraft engines of the same horsepower. The engine's low weight and tight packaging make for a light aircraft with minimal drag.

Hollow Grid Wing

The DarkAero 1 airframe uses a unique structural approach we call "Hollow Grid." Hollow Grid is an arrangement of CNC cut, honeycomb sandwich panel ribs and shear webs. All the compression, tension, and torsional loading is carried through the outer skin while the inner grid helps the skin maintain its shape and prevent buckling. This approach results in assemblies that are stronger and lighter when compared to many traditional structural approaches.

Simplified Build Process

The DarkAero 1 was designed to require only simple shop tools and no complex jigs or fixtures to complete. The carbon fiber composite airframe of the DarkAero 1 is formed using computer designed, precision CNC machined tooling. The end result is smooth, accurate parts that fit together with minimal sanding required to achieve final finishes.

Payload vs Range

All of these advantages combine to create an aircraft with exceptional speed and range, while maintaining a functional payload. The payload vs range chart below highlights the predicted capability of the aircraft.

The Kit Includes:

Airframe
Canopy
Engine Mount
Landing Gear
Control Hardware
Fittings and Fasteners
Kit Plans

Purchased Separately:

UL Power 520iS Engine
Avionics
Propeller
Wheels and Brakes
Paint
If you have additional questions about the DarkAero 1, check out our FAQ page here.



Milestones

Airframe & Systems

Airframe Structures
Airframe Structures
The majority of the DarkAero 1 prototype airframe is complete. This includes all major structures like the fuselage, wing, stabilizers, and landing gear. Remaining airframe tasks will focus on integrating and refining systems through the ground test program.
Primer Paint
Primer Paint
Primer paint has been applied to all external surfaces of the DarkAero 1 airframe. This protects the airframe structures from environmental hazards during the flight test program. Final top coat will be applied after flight testing.
Landing Gear Structures
Landing Gear Structures
Through the process of drop testing the DarkAero 1 prototype, the design of the main landing gear was refined and validated to handle expected operation loads.
Landing Gear Retract System
Landing Gear Retract System
The team is in the process of refining the landing gear actuation mechanism, emergency extend mechanism, and locking mechanism.
Nose Wheel Centering Mechanism
The DarkAero 1 utilizes a castering nose wheel. To prevent riding conditions during nose gear retract cycles, a self-centering mechanism will be designed, manufactured, and installed on the nose gear.
Firewall Forward
Firewall Forward
The cowling was not installed during initial engine tests to ensure proper air intake and cooling, but it will be installed for flight testing. Additional design and modification work on firewall-forward systems remains to maintain proper engine operation and cooling.
Control System
Control System
During initial control system testing, several areas for improvement were identified. Modifications are already underway to make the flight control system airworthy, allowing exploration of the full flight envelope during flight testing.
Cabin
Cabin
Several areas in the cabin require additional work to reach an airworthy state. These include updating the center console to house the fuel shutoff valve and routing fuel lines in this area. Positioning of the emergency gear extend controls is being finalized as well. Areas of the cabin floor will be built up to better handle wear from pilot ingress and egress.

Testing

Wing Proof Load Test
(Phase 1)
Wing Proof Load Test
The wing of the DarkAero 1 prototype was successfully tested to normal category loading conditions plus a safety factor.
Ground Vibration Tests
Ground Vibration Tests
The DarkAero 1 prototype underwent a series of ground vibration tests to determine if any hazardous airframe vibration modes exist within the flight envelope of the aircraft.
Low Speed Taxi Tests
Low Speed Taxi Tests
The DarkAero 1 prototype taxied under its own power for the first time, marking a key step toward flight readiness.
Test Pilot & Test Plan
Test Pilot & Test Plan
The team has chosen Sean Van Hatten of Initial Approach Aerospace to act as the test pilot for the DarkAero 1 prototype. The test area has been selected, and a test plan for first flights has been established. Sean has also provided feedback on the aircraft that led to refinement work prior to flight testing.
Fuel System Tests
Fuel System Tests
The DarkAero 1 does not use a fuel selector valve to switch between tanks, but instead uses a central sump plumbed with check valves to collect fuel and feed the engine. Testing of this system architecture was conducted to confirm that fuel could still flow from the sump throughout a range of bank angles and varying pressure conditions.
Horizontal Stabilizer Proof Load Test
Horizontal Stabilizer Proof Load Test
Like the wing, the horizontal stabilizer and empennage undergo a range of loads during flight maneuvers. These structures were successfully tested with simulated loads to confirm they can withstand flight conditions.
Control System Proof Load Tests
(Phase 1)
Control System Proof Load Tests
The team has completed initial load testing on all control surfaces on the DarkAero 1 prototype. These tests helped inform system changes that will be implemented and validated in a follow-up phase of tests.
Main Landing Gear Drop Tests
Main Landing Gear Drop Tests
Over 125 individual drops were conducted on the airframe and landing gear to explore their capability across a range of landing conditions.
Control System Proof Load Tests
(Phase 2)
After implementing changes to the control system that came out of the first phase of control system testing, the team will move on to final validation which includes compliance testing and proof loading of the control system. This will require applying the full range of flight loads plus a safety factor.
Retract System Cycle Tests
Retract System Cycle Tests
Following implementation of the latest design of the emergency extend system, the team will further test the gear to mitigate against failure modes and simulate a range of edge conditions the gear may encounter in flight.
Shock Tuning
Landing gear drop testing verified the landing gear structures are safe for flight. However, the main gear shocks still have room for improvement in rebound damping. Different shock assemblies will be tested off of the aircraft to allow continued work in parallel to other ground tests.
Wing Deflection Test
The elastic angular deflection of the wing root rib under load needs to be measured to accurately represent reaction loads on the wing attach lugs during the lug proof load test. Prior to completing this additional measurement-driven wing load test, the wing will undergo several updates to better accommodate the fuel line routing and flap control system mounts in the center spar area.
Wing Attach Lug Proof Load Test
The wing lugs provide the connecting interface between the wing and fuselage. Similar to the wing, the mounting lugs will be proof load tested to the same respective loads as the wing.
Vertical Stabilizer Proof Load Test
Like the wing and horizontal stabilizer, the vertical stabilizer and empennage undergo a range of loads during flight maneuvers. These structures will be tested with simulated stability and directional control loads to confirm they can withstand flight loading conditions.
Electrical System Tests
Isolated portions of the electrical system have already been tested. Additionally, the electrical system operated successfully throughout all initial engine run-ups and taxi tests. Prior to the first flights, the system will be more thoroughly tested to confirm that redundancies in the system work and that the harnesses and other hardware can successfully operate over longer periods of time.
High-Speed Taxi Tests
In the lead up to the first flight of the DarkAero 1, the aircraft will be tested down the runway at high enough speed to begin feeling out aerodynamic control response. This is the last major testing stage prior to achieving first flight.
First Flight
First Flight
The first flight will be conducted to establish basic control and flight characteristics of the aircraft.
Flight Test Campaign
Flight Test Campaign
Each stage of the flight test program will follow a pattern of gradually expanding the flight envelope by working through planned test cards. The goal is to explore the full flight envelope and confirm the flight characteristics expected for the mission of the DarkAero 1. The flight test program will be used to inform any additional changes that will be needed for DarkAero 1 production kits.
Gear Door Cycle Tests
The DarkAero 1 has retractable landing gear for improved aerodynamics during cruise. The gear door closing and opening system requires ground cycle testing prior to installation and actuation in flight.

Kit Production

Manufacturing Tools
Manufacturing Tools
The molds required for production of the major airframe structures of the DarkAero 1 are complete. Several molds may require changes as lessons are learned in the process of ground testing and flight testing.
Manufacturing Facility
Manufacturing Facility
The space to produce the first DarkAero 1 kits has been secured, and all equipment required to produce parts has been moved here. As engineering services contracts are expanded and kit production ramps up, additional space will be secured.
Manufacturing Team
The team is now at a size capable of producing DarkAero 1 kits at a rate of 5-10 per year. As the first set of kits are built and production processes are optimized, the team will be expanded to target a production output of 50 kits a year.
Manufacturing Process
The team has been able to further refine the manufacturing processes, workflow, and quality checks necessary to reliably produce the first DarkAero 1 kits. DarkAero built this capability through maintaining multiple different contract projects running in parallel to DarkAero 1 development. This has been important for better anticipating the challenges that will be associated with initial kit production.
Funding
To bring a new product like an aircraft to market, a “valley of death” must be crossed. This involves surviving the capital intensive development phase of the product before it can be sold profitably at scale. Completion of the first prototype is often mistaken as the valley exit, while the larger challenge of scaling manufacturing for production gets ignored. In the background, DarkAero has been quietly designing, building, and testing multiple aerospace vehicle platforms through its services business. This has been important for funding DarkAero 1 development, and also for building the capability to produce DarkAero 1 kits, allowing the “valley of death” to be crossed before the first kits are ever shipped while also eliminating the need for outside investment.
Scaled Manufacturing
DarkAero is planning to scale kit production to target a rate of 50 kits per year. This will require more optimized manufacturing workflows and a larger team. One of the primary goals of initial kit production will be to prove out whether current processes will scale to larger production volumes.

Reserve Now

Initial taxi testing of the DarkAero 1 has already begun, and we are working towards flight testing. Production of the first customer kits will follow the completion of flight testing. For the latest news on the program, check out our updates page: DarkAero Updates.

If you would like to reserve a production slot for a DarkAero 1 kit, we are accepting reservation deposits. The deposit is $1000 USD. Click the "Reserve Now" button below to contact us about placing a deposit.