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The thrust-to-weight ratio is calculated by dividing the thrust (in SI units – in newtons) by the weight (in newtons) of the engine or vehicle.The weight (N) is calculated by multiplying the mass in kilograms (kg) by the acceleration due to gravity (m/s 2).
The aircraft is designed to fly at up to 50,000 feet (15,200 m) and Mach 0.95, and capable of pulling a maximum of 9 g, while sustaining up to 4.5 g at about 20,000 feet (6,100 m). The Fury is to be powered by a single Williams FJ44-4M turbofan engine producing 4,000 pounds-force (17.8 kN) of thrust and has a maximum gross takeoff weight of ...
Comparison of major Chinese made military UAVs [49] Model Manufacturer Armaments Takeoff weight Engine type Maximum cruise speed Operational endurance CH-1 CASC: No 220 kg Piston 140 km/h 6 hours CH-2 CASC: No 220 kg Piston 160 km/h 8 hours CH-3 CASC: Yes, 80 kg 650 kg Piston 220 km/h 12 hours CH-4 CASC: Yes, 345 kg 1330 kg Piston 180 km/h
This variant is an uprated model of the 60-1 engines, with thrust increased to 3.7 kN (830 lbf). [2] TRI 60-2 071: This model powers the Aérospatiale C.22 target drone, and is slight uprated to 4.0 kN (900 lbf). TRI 60-2 074: This model powers several versions of the MQM-107 Streaker drone. TRI 60-2 077: This model powers the RBS-15 anti-ship ...
The Eurodrone is intended for long-endurance intelligence, surveillance and reconnaissance and ground support missions with precision-guided weapons. [3] The twin-turboprops are mounted in a pusher configuration behind the wing, similar to the smaller BAE Systems Mantis, and one-third larger than the MQ-9.
Unlike single- and double-rotor helicopters which use complex variable pitch rotors whose pitch varies as the blade rotates for flight stability and control, multirotors often use fixed-pitch blades; control of vehicle motion is achieved by varying the relative speed of each rotor to change the thrust and torque produced by each.
Data from Airforce Technology and Flight Global [1] [2] General characteristics. Capacity: 65.7 kg; Length: 13 ft 9 in (4.2 m) Wingspan: 11 ft 5 in (3.47 m) Width: 1 ft 10 in (0.57 m) Height: 1 ft 8 in (0.52 m) Gross weight: 1,499 lb (680 kg) Powerplant: 1 × Williams F107 turbofan engine, 700 lbf (3.1 kN) thrust; Performance. Maximum speed ...
A faster twin-jet engine version called the Banshee Jet 80 entered service in 2014, with a forward and side-looking infrared source in the nose to create, alongside the jet engines, a realistic rearward infrared target. It has a maximum airspeed of 180 m/s (650 km/h), and with an auxiliary fuel tank it has an endurance of over 45 minutes.