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60 kg (132.3 lb) Lightweight 62.5 kg (137.8 lb) Super Lightweight 65 kg (143.3 lb) Welterweight 67.5 kg (148.8 lb) Super Welterweight 70 kg (154.3 lb) Middleweight 72.5 kg (159.8 lb) Super Middleweight 75 kg (165.3 lb) Light Heavyweight 80 kg (176.4 lb) Heavyweight 90 kg (198.4 lb) Super Heavyweight Unlimited
The weighted arithmetic mean is similar to an ordinary arithmetic mean (the most common type of average), except that instead of each of the data points contributing equally to the final average, some data points contribute more than others.
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 ]
Adhesive weight: 54.0 t (53.1 long tons; 59.5 short tons) ... 5,500 kg (12,100 lb) coal: Water cap. 12.3 m 3 ... It was the same as the Sondermann variant after the ...
1986 variant powered by either two PW120A or PW121 engines and a 34,500 lb (15,650 kg) takeoff weight. DHC-8-103 1987 variant powered by two PW121 engines and a 34,500 lb (15,650 kg) takeoff weight (can be modified for a 35,200 lb [15,950 kg] take-off weight). DHC-8-102A 1990 variant powered by two PW120A engines with revised Heath Tecna interior.
700 kg (1,543.2 lb) The second-generation Nissan Sunny ( B110 ) was launched in January 1970 and was known as the Datsun 1200 in export markets. This new model was slightly larger in all dimensions to match its market rival, the equally popular Toyota Corolla .
Max takeoff weight: 82,000 lb (37,195 kg) [N 1] Fuel capacity: 3,580 imp gal (4,300 US gal; 16,300 L) in 6 wing tanks; Oil 150 imp gal (180 US gal; 680 L) in four nacelle tanks Powerplant: 4 × Rolls-Royce Merlin 85 or Packard-Merlin 68 V-12 liquid-cooled piston engines, 1,750 hp (1,300 kW) each
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.