FAZER
“A Pegasus. Made to go where you can’t.”
Next generation FAZER – More powerful, longer range.
FAZER-NEXT(Concept model)
- Operates autonomously
- A 70kg payload (twice of the FAZER R)
- Faster (MAX.150km/h), and longer range (120 minutes)
SPECIFICATIONS:
Item | Specification Value | |
Dimensions/Weight | Overall Length x Width x Height | 4,900 mm x 734 mm x 1,226 mm (16.1 feet x 2.4 feet x 4.0 feet) |
Max Takeoff Weight | 150 kg (330.7 lbs) | |
Engine | Engine Type/Cylinder Arrangement | 4-stroke, horizontally-opposed 2-cylinder engine |
Total Displacement | 390 cm3 (23.8 in3) | |
Maximum Output | 20.6 kW (27.6 hp) | |
Fuel Type/Fuel Tank Capacity | Regular gasoline/12 ℓ (3.2 gal) | |
Performance etc. | Operating Altitude (*1) | 3,000 m (9,842.5 feet) |
Payload (*1) | 70 kg (154 lbs) 20°C (68°F), 1 atmosphere |
|
Maximum Speed (forward airspeed) | 150 km/h (93.2 mi/h) | |
Cruising Speed | 100 km/h (62.1 mi/h) | |
Cruising Range(*2) | 200 km (124.3 miles) Optional Tank 600 km (372.8 miles) | |
Cruising Time(*2) | 120 minutes Optional Tank 6 hours |
*1 Operating altitude and payload are estimated with the fuel load at half (6 ℓ).
*2 Operating Range and cruising range are based on the use of a satellite transmitter-receiver.
FAZER R– Existing model
R-MAX and FAZER/FAZER R (Previous models)
- safe and cost effective solution
- 2,800 units of R-MAX and FAZER helping farmers in the USA, Japan and
other countries.
SPECIFICATIONS of FAZER R (Existing model):
Item | Specification Value | |
Dimensions/Weight | Overall Length x Width x Height | 3,665 mm x 734 mm x 1,226 mm (12.0 feet x 2.4 feet x 4.0 feet) |
Main Rotor Diametert | 3,115 mm (10.2 feet) | |
Tail Rotor Diameter | 550 mm (1.8 feet) | |
Max Takeoff Weight | 110 kg (242.5 lbs) | |
Engine | Engine Type/Cylinder Arrangement | Liquid-cooled, 4-stroke, OHV, 2-valve, horizontally-opposed 2-cylinder engine |
Total Displacement/ Bore x Stroke |
390 cm3/66.0 mm x 57.0 mm (23.8 in3 / 2.6 in x 2.2 in) |
|
Maximum Output | 20.6 kW (27.6 hp) at 6,000 r/min | |
Fuel Type/ Fuel Tank Capacity |
Regular gasoline/ 12ℓ (3.2 gal) |
|
Performance etc. | Operating Altitude (*1) | 2,800 m (9186.4 feet) |
Payload (*1) | 35 kg (77.2 lbs) 20°C (68°F), 1 atmosphere |
|
Maximum Speed (forward airspeed) |
20 m/s (44.7 mi/h) | |
Rate of Climb, Rate of Descent |
3 m/s, 3 m/s (9.8 feet/s) | |
Operating Range (*2) | 30 km (18.6 miles) | |
Cruising Range(*2) | 90 km (55.9 miles) | |
Cruising Time | 100 minutes |
*1 Operating altitude and payload are estimated with the fuel load at half (6ℓ).
*2 Operating Range and cruising range are based on the use of a satellite transmitter-receiver.
Proven reliability in remotely piloted helicopters
30 years of | experience and proven agricultural performance. |
2800+ units | are currently in use for pest control in over 2.6 million acres of rice fields across Japan every year. That accounts for one-third of all rice fields in Japan. |
Representing Yamaha's commitment to remain the leading force in remotely piloted helicopters designed for precision agriculture.
Proven reliability of autonomous helicopte
18 years of | autonomous helicopter experience |
At a distance of 1000+miles away |
Yamaha remotely controlled a FAZER via satellite communication in 2016 |
Since 2000, an autonomous version of R-MAX and FAZER R have been used in many applications for environmental research, disaster prevention and the study of post disaster research in places where humans cannot safely go.
Potential fields of operations to be proven
FAZER-NEXT
can carry a 70 kg(154 lbs) payload
has a 120 minutes flight time capacity
has an airspeed of 150 km/h(93 mph)
With outstanding UAV capability, the FAZER-NEXT allows a broad range of optional equipment payload to offer innovative aerial solutions for your business.
Demonstration flights
Autopilot system Development
AUTOPILOT PRECISION FEATURES
AUTOPILOT SAFETY FEATURES