Ducted Fan 'AirMule' UAS Completes First Phase of Flight Testing | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-06.23.25

Airborne-NextGen-06.24.25

AirborneUnlimited-06.25.25

Airborne-AffordableFlyers-06.26.25

AirborneUnlimited-06.27.25

Sun, Jan 17, 2010

Ducted Fan 'AirMule' UAS Completes First Phase of Flight Testing

Urban Aeronautics’ Rotorless VTOL Aircraft Demonstrates Hover Capability

The AirMule, a single-engine, VTOL Cargo and MedEvac UAS developed by Israel-based Urban Aeronautics, has successfully completed the first phase of its flight testing. This phase has consisted of tethered autonomous hovers with the vehicle’s Fly-By-Wire control system providing the necessary auto-stabilization in all three rotational axes of the vehicle ... pitch, roll and yaw.

Control of the vehicle is accomplished through a company developed, four channel, redundant flight control system that relies almost entirely on inertial measurements augmented by GPS for translational position and velocity readings. Height above ground is measured by two laser altimeters. 460 channels of telemetry provide real-time data to the ground based operators, enabling them to monitor the correct operation of the Turbomeca Arriel1 730 horsepower turbo-shaft engine as well as sub-systems.  These include the three company developed gearboxes, the two main lift rotors with their hydraulic pitch change mechanism and three uplink and downlink communication channels.

Results from the tests have confirmed the company’s predictions regarding power required for hover. The present hover height of approximately 2 feet is just outside of ground effect for this particular configuration. The aircraft uses a system of vanes for yaw and roll control, and in the test demonstrated the vehicle’s ability to perform hover with very high precision in gusty wind conditions (currently estimated and confirmed by the recent hover tests at 50 knots for the fully developed product).

Based on the success of these initial hover tests the vehicle is now being readied for the next phase which will include vehicle position stabilization in X,Y and height above ground.  During this upcoming phase the safety wires that are now connected to the tarmac will be removed.

FMI: www.urbanaero.com 

Advertisement

More News

NTSB Prelim: Piper PA-23

Pilot Also Reported That Due To A Fuel Leak, The Auxiliary Fuel Tanks Were Not Used On June 4, 2025, at 13:41 eastern daylight time, a Piper PA-23, N2109P, was substantially damage>[...]

ANN FAQ: Submit a News Story!

Have A Story That NEEDS To Be Featured On Aero-News? Here’s How To Submit A Story To Our Team Some of the greatest new stories ANN has ever covered have been submitted by our>[...]

Classic Aero-TV: One Man’s Vietnam

From 2023 (YouTube Edition): Reflections on War’s Collective Lessons and Cyclical Nature The exigencies of war ought be colorblind. Inane social-constructs the likes of racis>[...]

ANN's Daily Aero-Linx (07.03.25)

Aero Linx: Colorado Pilots Association (CPA) Colorado Pilots Association was incorporated as a Colorado Nonprofit Corporation in 1972. It is a statewide organization with over 700 >[...]

ANN's Daily Aero-Term (07.03.25): High Speed Taxiway

High Speed Taxiway A long radius taxiway designed and provided with lighting or marking to define the path of aircraft, traveling at high speed (up to 60 knots), from the runway ce>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC