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The Air Force uses 10% of the nation's aviation fuel. (JP-8 accounts for nearly 90% of its fuels.) This fuel usage breaks down as such: 82% jet fuel, 16% facility management and 2% ground vehicle/equipment. [4] To meet renewable energy goals, the Air Force plans to certify its entire fleet on coal-to-liquid synthetic fuel blends by 2011.
Engine: General Engine Products (GEP) V8, 6.5L Turbocharged Diesel [1] 190 hp (140 kW) [1] Payload capacity: M1151: 4,000 lb (1,800 kg) M1151A1: 3,950 lb (1,790 kg)
Class II – Supplies for which allowances are established by tables of organization and equipment, e.g., clothing, weapons, tools, spare parts, vehicles. Class III – Petroleum, oil and lubricants (POL) for all purposes, except for operating aircraft or for use in weapons such as flamethrowers, e.g., gasoline, fuel oil, greases, coal, and coke.
The Army expected the JLTV program to cut about five years off of the total program and save about US$5.9 billion, as Oshkosh's final competitive bid was low enough so the Army decided to "buy to budget" and get more platforms each year, which shrunk the total length of the contract and increased cost avoidances accrued each year.
With a weight of 3,500 kg (7,700 lb), the civilian Tigr-2 fuel consumption is 15 L/100 km. Its length is 5.7 m (19 ft), its width and height is 2.3 m (7.5 ft), and its ground clearance is 330 mm (1.08 ft). Compared with the military version, the civilian Tigr is 2,800 kg (6,200 lb) lighter.
The M915 has a 855 cu in (14.0 L) Cummins NTC 400 developing 400 hp (300 kW) at 2100rpm and 1,150 lbf⋅ft (1,559 N⋅m) of torque at 1500rpm. The M915A2 had a 775 cu in (12.7 L) Detroit Diesel Series 60 DDEC II developing 400 hp (300 kW) at 2100rpm and 1,400 lbf⋅ft (1,898 N⋅m) of torque at 1200rpm.
The Heavy Expanded Mobility Tactical Truck (HEMTT) is an eight-wheel drive, diesel-powered, 10-short-ton (9,100 kg) tactical truck. [2] The M977 HEMTT first entered service in 1982 with the United States Army as a replacement for the M520 Goer, and since that date has remained in production for the U.S. Army and other nations.
Data from General characteristics Type: turboshaft Length: 31.5 inches (0.80 m) Diameter: Dry weight: 315 pounds (143 kg) Components Compressor: low-pressure centrifugal, high-pressure centrifugal Turbine: low-pressure, high pressure, 2 power turbine Performance Maximum power output: 1,563 shp (1,166 kW) Specific fuel consumption: ~0.459 lb/(hp⋅h) (279 g/kWh) See also Comparable engines Avco ...