Title: LRC (train)
Content:  14000 lb less than a conventional low-speed loco. However, while development turned into production the weight grew to 245000 lb, eliminating any difference. By 1980, the National Research Council published a report noting that the weight had grown so much that service above 100 mph would cause unacceptable wear on the Corridor, thereby limiting the new LRC to the same speeds of the Turbo it was meant to replace. Alcan and TDC were also highly critical of Bombardier's management of the MLW portion of the program, suggesting that their mid-level management lacked the know-how to conclude the project rapidly.
Title: NAL Saras
Content:  speed of over 600 km/h, an endurance of six hours, a maximum flight altitude of 12 km (cruise altitude 10.5 km), short take-off and landing distances of about 600 m, a maximum rate of climb of 12 m/s, a low cabin noise of 78 dB, a range of 600 km with 19 passengers, 1,200 km with 14 passengers and 2,000 km with eight passengers, a high specific range of 2.5 km/kg and a low cost of operation of ₹ 5/km. While the designed empty weight of the aircraft is around 4,125 kg, the first prototype weighed in around 5,118 kg. This issue is sought to be addressed by including composite wings 
Title: KAI LAH
Content: Crew: 2 (pilots) ; Capacity: 2 x 20mm Magazines (Cabin) ; Length: 14.6 m (47.9 ft) ; Height: 4.35 m (14 ft 3 in) ; Empty weight: 3,400 kg (7,495 lb) ; Max takeoff weight: 4920 kg (10,847 lb) ; Powerplant: 2 x 1,024 shp turboshaft engines ; Main rotor diameter: 12.6 m (41 ft 4 in) ; Main rotor area: 124.7 m2 (1,342 sq ft) Max. speed: 243 km/h (151 m/h, 131 kn) ; Range: 857 km (533 mi, 463 nmi) ; Ferry range: 985 km (612 mi, 532 nmi) ; Service ceiling: 4,572 m (15,000 ft) ; Rate of climb: 8.9 m/s (1,750 ft/min) 1 × 20mm M197 electric cannon three-barreled electric Gatling-type rotary cannon ; 4 × "Chun-gum" Air-to-Ground Missile (2 on each side) or ; 2 × 7-shot rocket launcher Hydra 70 (1 launcher on each side) General characteristics  Performance  Armament 
Title: Hard Mobile Launcher
Content:  It can travel at speeds of up to 55 mph on the road and it also has off-road capabilities. The vehicle also has a trailer mounted plow which can be used to dig the launcher into the earth in order to help protect it were it within the vicinity of a nuclear detonation. The vehicle weighs a total of 108,400 kg (239,000 pounds), with a length of over 33.5m (110 feet) and it has the capability to transport objects weighing up to 36,300 kg (80,000 pounds). It is powered by a Rolls Royce Perkins diesel engine which produces 1200 hp and controls all 8 wheels using an electro-hydraulic transmission.
Title: Cessna Citation Longitude
Content:  the outer section. The six-passenger Latitude fuselage has been reinforced and stretched by another row of seats to accommodate eight people in double club. The manufacturer has not announced the final design weights (as of May 2016); BCA estimates a 24,000–25,000 lb. basic operating weight. Cabin height is 6.0 ft., width is 6 ft. 5 in., floor width is 4 ft. 1 in and cabin length is 25 ft. After a takeoff at 31,150 - 8,350 lb below the 39,500 lb MTOW, the climb rate is 2,550 ft/min at FL200. At its Mach 0.83, 473 kn TAS max cruise, fuel flow per side is 860-880 lb per hour at FL430 and ISA -4. A M0.79 long range cruise would burn 1,820 lb per hour at a 451 kn true airspeed for a 17,237 kg aircraft, and 2,122 lb per hour at its M0.84 MMO - 477 kn TAS.
Title: Rans S-12 Airaile
Content:  with Dacron covering introduced in 1991. Standard engine was the Rotax 447 of 40 hp, with the Rotax 503 of 50 hp and the Rotax 582 of 64 hp optional. Reported construction time 200 man-hours including complete cockpit fairing. Empty weight of 390 lb places the S-14 above the maximum category weight of the US FAR 103 Ultralight Vehicles category. Production completed with 125 completed by December 2004. ; S-17 Stinger ; Open-cockpit, conventional landing gear, single-seater, equipped with a standard Rotax 447 of 40 hp with the Rotax 503 of 50 hp optional. Empty weight of 249 lb places the S-17 within weight of the US FAR 103 Ultralight Vehicles category. 
Title: LARC-V
Content: Land speed: 30 mph ; Water speed: 	7.5 knots ; Capacity: 3 crew + 20 passengers (up to 10,000 lbs.) ; Maximum gradient: 60% ; Fuel capacity: 144 gallons diesel total (2 tanks) ; Unloaded land range: 280 to 335 miles ; Unloaded sea range: 110 miles 
Title: Flight planning
Content:  The weight of an aircraft is most commonly measured in kilograms, but may sometimes be measured in pounds, especially if the fuel gauges are calibrated in pounds or gallons. Many airlines request that weights be rounded to a multiple of 10 or 100 units. Great care is needed when rounding to ensure that physical constraints are not exceeded. When chatting informally about a flight plan, approximate weights of fuel and/or aircraft may be referred to in tons. This "ton" is generally either a metric tonne or a UK long ton, which differ by less than 2%, or a short ton, which is about 10% less.
Title: LARC-LX
Content:   It could carry up to 100 tons of cargo or 200 people, but a more typical load was 60 tons of cargo or 120 people. The vehicle was powered by four 265 hp GMC diesel engines positioned in the sides of the hull, each of which drove one wheel on land. Pairs of engines were coupled to drive each of the two 1.2 m-diameter propellers, which propelled the vehicle in the water. Its top speed was 20 mph on land, or 7.5 mph afloat. The operator occupied a small cab on the port side at the aft end of the vehicle. The LARC-LX was used to transport wheeled and tracked vehicles, including beach preparation equipment and 
Title: Land Rover 1/2 ton Lightweight
Content:  over the specified weight. The term Lightweight appears misleading as a standard 88 Land Rover weighed 1318 kg, but the higher total weight was due to the various frame reinforcement required for military usage. However, with the removable body panels taken-off it was below the limit. Since improvements to the helicopters meant more lift was available, the MoD accepted it for use. The main applications were actually to be shipped by cargo aircraft or stacked on train wagons, with helicopter transport a rare occurrence. The first production models were completed on 11 November 1968, and production continued until 1984.

Question: Verify the following claims with "True" or "False": The A-Rosa Luna weighs around 1850 tonnes and has a top speed of 24.0.
Answer: True