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Maximum speed : Mach 2.9 ... Kalibr and Onyx cruise missiles hit targets in Syria, ... Engine: ramjet, weight 200 kg, 4 tons of thrust; Range: ...
The FJ33 has a dry weight of less than 300 lb (140 kg), overall diameter of 18.36 in (466 mm), 38.43 in (976 mm) overall length, and produces between 1,000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust.
The components were designed to take the stresses of high-speed fighter aircraft ... Maximum thrust: Take-off: 10.79 kN (2,426 lbf) at 18,000 rpm; Maximum continuous ...
The thrust-to-weight ratio varies continually during a flight. Thrust varies with throttle setting, airspeed, altitude, air temperature, etc. Weight varies with fuel burn and payload changes. For aircraft, the quoted thrust-to-weight ratio is often the maximum static thrust at sea level divided by the maximum takeoff weight. [2]
The Pratt & Whitney PW2000, also known by the military designation F117 and initially referred to as the JT10D, is a series of high-bypass turbofan aircraft engines with a thrust range from 37,000 to 43,000 lbf (160 to 190 kN).
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 Aerospatiale 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 ...
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio
The TJ100 engine entered service in 2003, [1] and is the most popular of PBS's turbojet engines as more than 1,000 engines have been sold to 40 countries worldwide. [2] The engine has been developed for unmanned aerial vehicles , including target drones , remote carriers, unmanned combat aerial systems , light experimental jet aircraft , and ...