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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.
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.
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)
JP-8, or JP8 (for "Jet Propellant 8"), is a jet fuel, specified and used widely by the US military.It is specified by MIL-DTL-83133 and British Defence Standard 91-87, and similar to commercial aviation's Jet A-1, but with the addition of corrosion inhibitor and anti-icing additives.
Typical land speeds are approximately 100 km/h (62.5 mph) in either 4- or 8-wheel drive; however, fuel economy decreases in 8-wheel drive. The vehicles operate on diesel fuel . They are equipped with a 25 mm M242 Bushmaster autocannon, two 7.62 mm M240 machine guns , and two four-barrel smoke grenade launchers located on the forward left and ...
In addition to 3,000-shp output, the targets for AATE were a 25% reduction in fuel consumption (less than 0.347 lb/(hp⋅h), 211 g/kWh), a 65% improvement in power to weight (more than 6.5 hp/lb, 10.7 kW/kg), a 20% improvement in design life (more than 6000 hours and 15000 cycles), a 35% reduction in production (less than $650k per engine) and maintenance cost, and a 15% reduction in product ...
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.
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 ...