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Ukrspecsystems PD-2 is a Ukrainian multi-purpose unmanned aerial vehicle (UAV). It is designed for aerial reconnaissance and for combat use as a carrier of bombs with warheads weighing up to 3 kg (6.6 lb). [1] The aircraft can take off from a runway, or be equipped with removable modules for vertical take-off and landing.
2 Mb 1028 Kb STM32F103 N/A ADIS16470 acc/gyro ISM20649 acc/gyro BMI088 acc/gryo RM3100 mag MS5611 x2 baro Discontinued - replaced by X7+ Pro Cube Black Hex/Proficnc Ardupilot PX4 CubePilot STM32F427 168 MHz 2 Mb 256 Kb STM32F100 N/A LSM303D acc/mag L3GD20 gyro MS5611 baro Cube Black (Pixhawk 2.1) Hex/Proficnc Ardupilot PX4 FMUv3 STM32F427
Bristol Siddeley BS.1006 Bristol Siddeley M4 research ramjet. Became R.2 research engine. Bristol Siddeley BS.1007; Bristol Siddeley BS.1008 Bristol Siddeley M1.2 ramjet. Bristol Siddeley BS.1009 Bristol Siddeley M3 ramjet. Modified BT.3 Thor intended for proposed Bloodhound III. Modified nozzle, intake and diffuser. [10] Bristol Siddeley BS.1010
Rotax is one of the world's principal suppliers of aircraft engines for ultralight aircraft, light aircraft and unmanned aerial vehicles. [2] Between 1985 and 1995, 60,000 Rotax engines were sold for aircraft propulsion. [2] In the light aircraft class, in 1998 Rotax outsold all other aero engine manufacturers combined. [4]
However, with a manual transmission engine RPM can redline in "neutral", or by shifting to a higher gear too late, or by shifting to a lower gear too early. In the case of "neutral" or shifting up too late, a rev limiter can easily keep engine RPM below the redline. If a manual transmission is shifted down too early, the speed of the vehicle ...
Data from OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582 General characteristics Type: two-stroke air-cooled aeroengine Bore: 67.5 mm (2.66 in) Stroke: 61 mm (2.4 in) Displacement: 426.5 cc (26.64 cu in) Dry weight: 26.8 kg (59 lb) (dry, no exhaust system) Components Valvetrain: piston ports Fuel system: pneumatic pump pressurized Fuel type: regular autofuel Oil system: premixed in the fuel ...
The Wing Loong II UAV MALE is an enlarged version of the Wing Loong I with a longer body and wider wing span. It has a slender fuselage, V-tail , and ventral fin. The aircraft features retractable landing gear, including two main wheels under the fuselage and one single wheel under the nose.
compressor speed [1] N 1, N 2, etc. refers to the specific compressor spool (in the order that air passes over them). (See: Jet engine) N g: gas generator speed [1] N h: high rotor speed [1] N p: power turbine speed [1] N r: rotor speed (helicopters)