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The Short SC.1 was a single-seat low wing tailless delta wing aircraft of approximately 8,000 lb all-up weight (max. 7,700 lb for vertical flight). [3] It was powered by four vertically-mounted, lightweight Rolls-Royce RB.108 lift engines that provided a total vertical thrust of 8,600 lb, along with a single RB.108 cruise engine in the rear of ...
The following month, the Lancaster's official all-up (maximum take-off) weight was increased from 60,000 lb to 63,000 lb, and after mid-1943, when the limit was raised to 65,000 lb, Lancasters would seldom carry less than an 8,000 lb bomb load, even when fully fuelled to 2,154 gallons for maximum range. [19]
Data from Jane's All the World's Aircraft 1988–1989 General characteristics Crew: 3 (2 pilots plus 1 cabin crew) Capacity: 30 passengers, or 18 Litter based passengers / 7,000 lb (3,175 kg) maximum payload Length: 58 ft 0.5 in (17.691 m) Wingspan: 74 ft 8 in (22.76 m) Height: 16 ft 3 in (4.95 m) Wing area: 453 sq ft (42.1 m 2) Airfoil: root: NACA 63A418 ; tip: NACA 63A414 Empty weight ...
up to 8,000 lb (3,600 kg) internally in nacelle bomb-bays + up to 8,000 lb (3,600 kg) externally under the wings 4 × 2,160 lb (980 kg) torpedoes or; 4 × 2,000 lb (907 kg) mines or bombs or; 8 × 1,000 lb (454 kg) mines or; 16 × 500 lb (227 kg) bombs or; 16 × 330 lb (150 kg) depth charges or; 1 × Mark 90 nuclear bomb nuclear depth charge ...
The hull was made from 2.5-inch (6.4 cm) thick transparent acrylic, Poly(methyl methacrylate), and housed a crew of two (pilot and observer). Operational subsystems included a main lead acid battery power supply, electrical distribution and control circuitry, a hydraulic system to operate a self-contained winch/anchor system, and two side ...
4 x 20.2 Convertiplanes. MTOW = Maximum take-off weight. Type MTOW [kg] Power output [kW] Power to weight [W/kg] Rotor diameter [m] Bell Boeing V-22 Osprey:
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