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An early version of the Edge 540 with a wire-braced tail. The Zivko Edge 540 manufactured by Zivko Aeronautics is a highly aerobatic aircraft.Capable of a 420 degree per second roll rate and a 3,700 foot per minute climb rate, it has been flown to victory on the international Unlimited aerobatics circuit several times since the mid-1990s.
The F1 Rocket is a tandem two-seat low-wing cantilever monoplane built mainly in aluminum. [1] The Rocket has a titanium fixed conventional landing gear with a tailwheel. . Designed to be built with a range of nose-mounted engines between 235 and 350 hp (175 and 224 kW) the prototype has a Lycoming IO-540 with a three-bladed propelle
The SG 540 is a 5.56×45mm NATO assault rifle developed in the early 1970s by Schweizerische Industrie Gesellschaft (SIG, currently SAN Swiss Arms AG) of Neuhausen, Switzerland [4] as a private venture primarily destined for export markets and as a potential replacement for the 7.5×55mm Swiss SG 510 automatic rifle known as the Stgw 57 in Swiss service.
SG 550 disassembled into its main constituent groups. The SG 550 is a selective-fire 5.56×45mm NATO assault rifle firing from a closed bolt. It has a gas-actuated piston-driven long-stroke operating system derived from the SIG SG 540 series of rifles, which uses burnt powder gases vented through a port in the barrel to power the weapon's ...
Data from Jane's all the world's aircraft 1976–77. General characteristics Crew: Two Capacity: four passengers Length: 36 ft 9.75 in (11.22 m) Wingspan: 49 ft 0.5 in (14.95 m) Height: 14 ft 6 in (4.42 m) Wing area: 255 sq ft (23.69 m 2) Aspect ratio: 9.45:1 Airfoil: NACA 23012 modified Empty weight: 4,635 lb (2,102 kg) Max takeoff weight: 6,750 lb (3,062 kg) Powerplant: 2 × Lycoming IO-540 ...
Data from Jane's All The World's Aircraft 2003–2004 General characteristics Crew: 2 Capacity: 4 passengers Length: 10.93 m (35 ft 10 in) (fuselage length), 12.94 m (42 ft 6 in) (overall length, rotors turning) Height: 3.34 m (10 ft 11 in) Empty weight: 1,220 kg (2,690 lb) Max takeoff weight: 2,250 kg (4,960 lb) Fuel capacity: 540 L (143 US Gal) Powerplant: 1 × Turbomeca Arriel 2B turboshaft ...
Stretched from the Citation I, the Model 550 was announced in September 1976, first flew on January 31, 1977, and was certified in March 1978. The II/SP is a single pilot version, the improved S/II first flew on February 14, 1984 and the Citation Bravo , a stretched S/II with new avionics and more powerful P&WC PW530 A turbofans, first flew on ...
The R.550 Magic (backronym for Missile Auto-Guidé Interception et Combat [1] [2]) is a short-range air-to-air missile designed in 1965 by French company Matra to compete with the American AIM-9 Sidewinder, and it was made backwards compatible with the Sidewinder launch hardware.
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