2023/24: Orange hornet
P1
ASIA-PACIFIC
P1
AUSTRALIA
P2
INTERNATIONAL
P10
OVERALL
ORANGE HORNET
Orange Hornet was the USYD DBF Team’s second entry into the DBF Competition, building on the strong first entry from the previous year. Going into the season, the team committed to improving results, taking risks and proving the capabilities of the Australian UAV industry to the world. Orange Hornet is a testament to the dedicate of the 40 engineers that contributed to it.
competition rules
The 28th Annual AIAA DBF Competition was organised by Textron Aviation, focusing on civilian applications with the theme of Urban Air Mobility. As a result, the competition focused on Short Take-Off Capabilities, and maximising payload carrying capacity. Aligned with the Urban Air Mobility theme, the aircraft had to be engineered to be capable of efficient transportation of ‘medical supplies’ and ‘passengers’ per competition requirements.
- 20ft. (~6m) max take-off distance
- 5ft. (~1.5m) max wingspan
- 2.5ft. (0.75m) wide parking space that the aircraft had to be configured to fit in
- 5 minute time limit on parking to flight transition and payload installation for all missions
Mission 1
- Delivery Flight
- Complete 3 laps in 5 minute flight window
- Pass/Fail score
- Medical Transport Flight
- Complete 3 laps as quick as possible
- Carry as much weight as possible inside aircraft
- Score was a function of the weight carried and the time taken to complete 3 laps
- Urban Taxi Flight
- Complete as many laps as possible in 5 minutes
- Carry as many passengers (wooden craft dolls) as possible
- Score was a function of the passenger carried, laps completed, and the battery capacity
- Configuration Demonstration
- Timed transition of aircraft from parking to flight configuration
- Score was dependent
KEY HIGHLIGHTS
1.5 metre wingspan
2.0 metre fuselage length
3.5 Aspect Ratio
120N Static Thrust
HIGH LIFT DEVICE: Slotted Brown flaps
PARKING: Swivel wing mechanism
STALL SPEED: 40 KM/HR
TOP SPEED: 140 KM/HR
design
Orange Hornet is a high-wing conventional body aircraft designed for short ground-rolling take-off and capable of accommodating high payload capacity. To produce the 14kg target thrust, the propulsion system utilises a tractor configuration with twin motors mounted on the wing. With a wingspan of 1.5m and aspect ratio of 3.5, the rectangular wing incorporates slotted flaps for an enhanced lift coefficient at take-off. The design also features a T-tail empennage to maximise the elevator effectiveness and a tricycle undercarriage configuration for maximum take-off and landing stability. An efficient wing swivelling mechanism has been engineered to enable the aircraft to rapidly transition between flight configuration and a parking configuration that fits within a 2.5ft parking spot.
PROJECT LEADS
PROJECT DIRECTOR
JOANNA LIU
PROJECT DIRECTOR
JOSHUA KALLARACKEL
CHIEF ENGINEER
JACOB JAMES
MANUFACTURING DIRECTOR
HUGH DILLON
AEROSTRUCTURES LEAD
KYLE MAYES
AEROSTRUCTURES LEAD
travis Giannarakis
PAYLOAD LEAD
JESSICA SONG
PAYLOAD LEAD
JOSEPH DIONG
FLIGHT PERFORMANCE LEAD
JOSHUA KAY
FLIGHT PERFORMANCE LEAD
ANNA LEE