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Data from Jane's All the World's Aircraft 2010-11 General characteristics Crew: 1 Capacity: 3 pax Length: 6.61 m (21 ft 8 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.6 m (8 ft 6 in) Wing area: 11 m 2 (120 sq ft) Empty weight: 336 kg (741 lb) Max takeoff weight: 600 kg (1,323 lb) Max useful weight: 269 kg (593 lb) Powerplant: 1 × Rotax 912 ULS 4-cylinder air-cooled horizontally-opposed piston ...
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Apollo Launch Escape System diagram. If the rocket failed in the last five minutes before launch, the CM and the launch escape system (LES, see figure) would separate from the remainder of the rocket below with the LES propelling itself and the CM beneath it upward and eastward to the sea using a small solid-fueled motor (the launch escape motor) at the top of the tower on the launch escape ...
The AN/PRC-153 is the Joint Electronics Type Designation System designation for the US military version of the Motorola XTS-2500i secure handheld 2-way radio, known as the Integrated, Intra-Squad Radio (IISR) within the US Marine Corps. [1]
Template talk: Bravo programming. ... Download QR code; Print/export Download as PDF; Printable version; In other projects ...
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