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)
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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.
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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.
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1 hectare in about 6 minutes
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Use the downwash effects from 3 to 4m height
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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.
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by NHK (Japan Broadcasting Corporation)
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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.
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Demonstration flights
Autopilot system Development
AUTOPILOT PRECISION FEATURES
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AUTOPILOT SAFETY FEATURES
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