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For a variety of reasons (largely historical), weight classes of the same name can be of vastly different weights. For example, a boxing middleweight weighs up to 72 kg (160 lb), an ISKA middleweight upper limit is 75 kg (165 lb), and a K-1 middleweight upper limit is 70 kg (154 lb).
It was the same as the Sondermann variant after the conversion of the latter. These locomotives could haul a train of 820 tons at a speed of 50 km/h and even attained a speed of 40 km/h with a 1,390 ton train. On a line with a 0.5% incline they could manage an 845-ton train at 25 km/h.
It has a curb weight of 4,950 lb (2,250 kg) and a payload of 1,250 lb (570 kg); the estimated driving range is 50 mi (80 km) and the maximum speed is 60 mph (97 km/h). Testing at EVTC showed the ECRV met or exceeded its performance requirements, including an accelerated 20,000 mi (32,000 km) reliability test. [ 29 ]
1992 variant powered by two PW121 engines and a 36,300 lb (16,450 kg) takeoff weight. DHC-8-100PF DHC-8-100 converted to a freighter by Voyageur Aviation, with a 10,000 lb (4,536 kg) cargo capacity. [44] DHC-8M-100 Two aircraft for Maritime Pollution Surveillance, operated by Transport Canada, equipped with the MSS 6000 Surveillance system. [45 ...
As Bruce Banner, the character is about 5 ft 9 in (1.75 m) tall and weighs 128 lbs (58.05 kg), but when transformed into the Hulk, the character stands between 7 and 8 ft (2.13 - 2.43 m) tall and weighs between 1,040 and 1,400 lbs (471.73 - 635.02 kg).
For example, the FAO (2002) figure for Denmark, which has one of the highest meat export rates compared to its population, was 145.9 kg (322 lb) (highest in the world). More recent FAO figures (2009) have taken the earlier discrepancy into account, resulting in a significantly lower 95.2 kg (210 lb) for Denmark (13th in the world).
Falcon Heavy has the second highest lift capability of any operational rocket, with a payload of 63,800 kg (140,700 lb) to low Earth orbit, 26,700 kg (58,900 lb) to Geostationary Transfer Orbit, and 16,800 kg (37,000 lb) to trans-Mars injection. [66] The rocket was designed to meet or exceed all current requirements of human rating.
In 1940, for a "military load" of 1,500 lb (680 kg), the Royal Aircraft Establishment (RAE) had advised that work on an aircraft of 8,500 lb (3,900 kg) all-up weight, with a total static thrust of 3,200 lbf (14 kN) should be started, with an 11,000 lb (5,000 kg) design for the expected, more powerful, W.2 and axial engine designs. George Carter ...