Thrust-specific fuel consumption (TSFC) is the fuel efficiency of an engine design with respect to thrust output. TSFC may also be thought of as fuel...
13 KB (1,051 words) - 07:03, 5 March 2024
Brake-specific fuel consumption (BSFC) is a measure of the fuel efficiency of any prime mover that burns fuel and produces rotational, or shaft power...
32 KB (1,528 words) - 23:52, 20 July 2024
efficiency within a shaft engine Thrust-specific fuel consumption, fuel efficiency of an engine design with respect to thrust output This disambiguation page...
290 bytes (74 words) - 06:44, 9 June 2019
and with improved engine brake-specific fuel consumption and propulsive efficiency or thrust-specific fuel consumption. Endurance and range can be maximized...
123 KB (7,662 words) - 19:13, 10 May 2025
by a two-stage, air-cooled, HP turbine. This engine has a thrust-specific fuel consumption (TSFC) of 0.39 lb/(lbf⋅h) (11 g/(kN⋅s)) at static sea level...
24 KB (2,188 words) - 14:04, 7 January 2025
is usually placed before "specific" in the full term (e.g., "thrust-specific fuel consumption"). Named and unnamed specific quantities are given for the...
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energy Standard gravity Thrust specific fuel consumption—fuel consumption per unit thrust Specific thrust—thrust per unit of air for a duct engine Heating...
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provides a lower fuel consumption for the same thrust, measured as thrust specific fuel consumption (grams/second fuel per unit of thrust in kN using SI...
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Range (aeronautics) (redirect from Specific range)
force in newtons Jet engines are characterized by a thrust specific fuel consumption, so that rate of fuel flow is proportional to drag, rather than power...
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low specific thrust (~30 lbf/(lb/s)) to reduce noise, and to reduce fuel consumption, because a low specific thrust helps to improve specific fuel consumption...
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terms of its output power Thrust specific fuel consumption (TSFC), the fuel efficiency of a jet engine design in terms of its thrust efficiency Super Famicom...
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Internal combustion engine (redirect from Fossil fuel vehicle)
energy efficiency fuel/propellant consumption (brake specific fuel consumption for shaft engines, thrust specific fuel consumption for jet engines) power-to-weight...
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Thrust reversal, also called reverse thrust, is the temporary diversion of an aircraft engine's thrust for it to act against the forward travel of the...
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increases thrust as an alternative to using a bigger engine with its added weight penalty, but at the cost of increased fuel consumption (decreased fuel efficiency)...
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long-range derivative with a 0.526 lb/lbf/h (14.9 g/kN/s) cruise Thrust-specific fuel consumption; and could replace the 16-tf PS-90A powering the Tupolev Tu-204/214...
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case of the rocket, there is a direct relation between specific impulse, specific fuel consumption and exhaust velocity. This direct relation is not generally...
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50:1, and a bypass ratio higher than 6.5:1 for a 3–5% better thrust specific fuel consumption. After flight tests, G700 bested its competitor's 7,700 nmi...
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Variable cycle engine (section Specific thrust)
reduce aircraft drag at supercruise, SST engines require a high specific thrust (net thrust/airflow) to minimize the powerplant's cross-sectional area. This...
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Turbojet (section Thrust augmentation)
pressure thrust. The rate of flow of fuel entering the engine is very small compared with the rate of flow of air. If the contribution of fuel to the nozzle...
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000 lbf (4,400 N) and 1,800 lbf (8,000 N) static thrust. Specific fuel consumption at 1,200 lbf (5,300 N) thrust (SLS, ISA) is understood to be 0.486 lb/(lbf⋅h)...
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Ramjet (redirect from Solid-fueled ramjet)
has the advantage of giving thrust even at zero speed. In a solid fuel integrated rocket ramjet (SFIRR), the solid fuel is cast along the outer wall...
37 KB (4,945 words) - 15:05, 24 April 2025
Blade pitch (section Reverse thrust)
performance and fuel economy. It is quite common for an aircraft to be designed with a variable-pitch propeller, to give maximum thrust over a larger speed...
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flight engineer, or autopilot to control the thrust output of the aircraft's engines, by controlling the fuel flow to those engines. Throttle levers are...
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Rocket engine (section Thrust vectoring)
are the lightest and have the highest thrust, but are the least propellant-efficient (they have the lowest specific impulse). The ideal exhaust is hydrogen...
101 KB (11,723 words) - 04:43, 8 May 2025
Jet engine performance (redirect from Thrust lapse)
jet engine company sells' and, as such, criteria include thrust, (specific) fuel consumption, time between overhauls, power-to-weight ratio. Some major...
119 KB (16,982 words) - 10:11, 2 April 2025
produced 20,000 kgf (44,000 lbf; 200,000 N) thrust at take-off and had a cruise thrust-specific fuel consumption of 1.22 kg/(kgf. h). which gave the aircraft...
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Components of jet engines (section Thrust reversers)
Afterburner or reheat (British) — (mainly military) Produces extra thrust by burning fuel in the jetpipe. This reheating of the turbine exhaust gas raises...
47 KB (6,819 words) - 22:42, 24 March 2025
fuel burn gain margin of 5–7% over the next decade, averaging 1% per year combined with gear ratio tweaks. The PW1400G has a cruise thrust-specific fuel...
93 KB (8,358 words) - 13:44, 9 May 2025
construction, and high noise levels. While the thrust-to-weight ratio is excellent, thrust specific fuel consumption is very poor. The pulsejet uses the Lenoir...
28 KB (3,804 words) - 13:37, 6 May 2025