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Unit of force
the free dictionary. The pound of force or pound-force (symbol: lbf, sometimes lbf,) is a unit of force used in some systems of measurement, including
Pound_(force)
Topics referred to by the same term
LBF or lbf may refer to: Lingbao railway station (China Railway telegraph code: LBF), a railway station in Sanmenxia, Henan, China North Platte Regional
LBF
Unit of pressure or stress
(abbreviation: psi) or, more accurately, pound-force per square inch (symbol: lbf/in2), is a unit of measurement of pressure or of stress based on avoirdupois
Pound_per_square_inch
Unit of energy
The foot-pound force (symbol: ft⋅lbf, ft⋅lbf, or ft⋅lb ) is a unit of work or energy in the engineering and gravitational systems in United States customary
Foot-pound
at 5,000 rpm; 200 N⋅m (148 lbf⋅ft) at 1,500–4,000 rpm — CMBA, CPVA 92 kW (125 PS; 123 bhp) at 5,000 rpm; 200 N⋅m (148 lbf⋅ft) at 1,500–4,000 rpm — CZCA
List of Volkswagen Group petrol engines
List_of_Volkswagen_Group_petrol_engines
DIN-rated power & torque output 55 kW (75 PS; 74 bhp) at 4,200 rpm; 180 N⋅m (133 lbf⋅ft) at 2,000 rpm applications 2009- Volkswagen Polo Mk5 (BlueMotion model
List of Volkswagen Group diesel engines
List_of_Volkswagen_Group_diesel_engines
Centrifugal-flow turbojet engine
greater thrust, starting at 4,000 lbf (18 kN) and ending at 4,600 lbf (20 kN) with an additional low-altitude boost to 5,400 lbf (24 kN) with water-alcohol injection
Allison_J33
Turbojet aircraft engine
Military versions produce up to 3,500 lbf (16 kN) of thrust dry; afterburning variants can reach up to 5,000 lbf (22 kN). The engine, depending upon additional
General_Electric_J85
Turbojet engine
in the early 1950s. The J57 (first run January 1950) was the first 10,000 lbf (45 kN) thrust class engine in the United States. It is a two-spool engine
Pratt_&_Whitney_J57
Unit of mass
of one pound (lbf) is exerted on it. 1 slug = 1 lbf ⋅ s 2 ft ⟺ 1 lbf = 1 slug ⋅ ft s 2 {\displaystyle 1~{\text{slug}}=1~{\text{lbf}}{\cdot }{\frac
Slug_(unit)
Unit of power
t = 180 lbf × 2.4 × 2 π × 12 ft 1 min = 32,572 ft ⋅ lbf min . {\displaystyle P={\frac {W}{t}}={\frac {Fd}{t}}={\frac {180~{\text{lbf}}\times 2
Horsepower
Jet-powered executive transport aircraft
two Turboméca Marboré turbojets of 880 lbf (3.9 kN) thrust, although most aircraft were later upgraded to 1,058 lbf (4.71 kN) units. The aircraft seated
Business_jet
Turbojet engine
axial-flow turbojet engine first flown in 1955. A two-spool design in the 17,000 lbf (76 kN) thrust class, the J75 was essentially the bigger brother of the Pratt
Pratt_&_Whitney_J75
Turbofan aircraft engine
thrust-specific fuel consumption (TSFC) of 0.39 lb/(lbf⋅h) (11 g/(kN⋅s)) at static sea level takeoff and 0.64 lb/(lbf⋅h) (18 g/(kN⋅s)) at a cruise speed of Mach
Rolls-Royce_BR700
High-thrust turbofan jet engine
decreased by 15,800 lbf (70 kN) to a new rating of 99,500 lbf (443 kN) per engine. The engine for the 777-8X was to be derated to 88,000 lbf (390 kN). The engine
General_Electric_GE9X
to 12.5 kg⋅m (123 N⋅m; 90 lbf⋅ft) while having a dry weight of 58.6 kg (129.2 lb). Rated up to 15.5 kg⋅m (152 N⋅m; 112 lbf⋅ft) while having a dry weight
List_of_Hyundai_transmissions
Unit of torque
A pound-foot (lb⋅ft), abbreviated from pound-force foot (lbf · ft), is a unit of torque representing one pound of force acting at a perpendicular distance
Pound-foot
Aircraft engine
turbofan engine produced by Honeywell Aerospace. Rated in the 6,540–7,624 lbf (29.09–33.91 kN) range, the HTF7000 is used on the Bombardier Challenger
Honeywell_HTF7000
American low-bypass turbofan
given in foot-pounds (lbf) and kilonewtons (kN). XTF30-P-1 8,250 lbf (36.70 kN) YTF30-P-1 TF30-P-1 8,500 lbf (37.81 kN) / 18,500 lbf (82.29 kN) with afterburner
Pratt_&_Whitney_TF30
Small turbofan engine
started in 1992 with the 1,900 lbf (8.5 kN) thrust FJ44-1A. The FJ44-1C is derated to 1,500 lbf (6.7 kN). The uprated to 2,300 lbf (10 kN) FJ44-2A was introduced
Williams_FJ44
Family of turbofan engines used by the Soviet military
now NPO Saturn in Russia, originally as a 12.5-tonne (122.6 kN, 27,560 lbf) powerplant for the Sukhoi Su-27 long range air superiority fighter. The
Saturn_AL-31
Family of turbofan aircraft engines
architecture of the 1972 RB211 with a maximum thrust ranging from 61,900 to 97,000 lbf (275 to 431 kN). Launched as the RB-211-524L in June 1988, the prototype
Rolls-Royce_Trent
Turbofan engine
was introduced in 1971 at 2,200 lbf (9,800 N) thrust, and has since undergone a series of upgrades to just over 3,000 lbf (13 kN) thrust in the latest versions
Pratt_&_Whitney_Canada_JT15D
High-bypass turbofan aircraft engine
thrust ranging from 50,000 to 99,040 lbf (222 to 441 kN), it is used on many wide-body aircraft. The 52,000–62,000 lbf (230–275 kN), 94 in (2.4 m) -fan PW4000
Pratt_&_Whitney_PW4000
54 bhp) at 4,750 rpm; 108 N⋅m (80 lbf⋅ft) at 3,000 rpm — AWY, BMD 44 kW (60 PS; 59 bhp) at 5,000 rpm; 108 N⋅m (80 lbf⋅ft) at 3,000 rpm — BBM DIN-rated
List of discontinued Volkswagen Group petrol engines
List_of_discontinued_Volkswagen_Group_petrol_engines
1940s British turbojet aircraft engine
7,350 lbf (32,700 N) thrust in the de Havilland Comet C.2, the RA.14/Mk.201, 9,500 lbf (42 kN) in the Vickers Valiant and the RA.26, 10,000 lbf (44 kN)
Rolls-Royce_Avon
Axial-flow compressor jet engine
000 lbf (22 kN) J35-A-21 Similar to -35, 5,600 lbf (25 kN) / 7,400 lbf (33 kN) with afterburner J35-A-21A Similar to -35, 5,600 lbf (25 kN) / 7,400 lbf (33 kN)
Allison_J35
Family of turbofan aircraft engines
JT3D-1 17,000 lbf (75.62 kN) thrust civil version, (Water injection optional) JT3D-2 (TF33-P-3) 17,000 lbf (75.62 kN) JT3D-3 18,000 lbf (80.07 kN), (Water
Pratt_&_Whitney_JT3D
Rifle cartridge
Silvertip ammunition (SBST338) retains over 1,600 ft⋅lbf (2,200 J) at 625 yd (572 m) and has 1,000 ft⋅lbf (1,400 J) energy at 800 yd (730 m). Winchester's
.338_Winchester_Magnum
High-bypass turbofan aircraft engine
engine, until being surpassed in January 2020 by its successor, the 110,000 lbf (490 kN) GE9X, which has a larger fan diameter by 6 inches (15 cm). However
General_Electric_GE90
Turbojet engine
850 lbf (12.7 kN) thrust CJ610-2B 2,400 lbf (11 kN) thrust CJ610-4 2,850 lbf (12.7 kN) thrust CJ610-6 2,950 lbf (13.1 kN) thrust CJ610-8A 2,950 lbf (13
General_Electric_CJ610
Turbofan aircraft engine
Rolls-Royce Trent, with a 3 m (120 in) fan, an IP and HP spool. The 84,200–97,000 lbf (375–431 kN) engine has a 9.6:1 bypass ratio and a 50:1 pressure ratio. It
Rolls-Royce_Trent_XWB
High-bypass turbofan engine
the thrust range from 23,500 lbf to 33,000 lbf: The 23,500 lbf (105 kN) thrust V2524-A5 for the Airbus A319 The 24,800 lbf (110 kN) thrust V2527-A5 for
IAE_V2500
Four-engined twin-aisle airliner family
similar airframe to the A330-200/300. Differences include four 151 kN (34,000 lbf) CFM56s instead of two high-thrust turbofans to bypass ETOPS restrictions
Airbus_A340
Reciprocating internal combustion engine
Output is 340 hp (254 kW; 345 PS) at 6,400 rpm with 46 kg⋅m (451 N⋅m; 333 lbf⋅ft) of torque at 4,000 rpm. Redline is at 6,600 rpm. It has an aluminum engine
Nissan_VK_engine
Airport in North Platte, Nebraska, USA
North Platte Regional Airport (IATA: LBF, ICAO: KLBF, FAA LID: LBF) (Lee Bird Field) is a public airport three miles east of North Platte, in Lincoln
North_Platte_Regional_Airport
Measure of torque on geartrains
Effective torque (often referred to as wheel torque or torque to the wheels) is a concept primarily associated with automotive tuning. Torque can be measured
Effective_torque
Reciprocating internal combustion engine
7 mm (2.74 in); 12v DOHC. It produces 56.6 kW (77 PS; 76 hp) and 98 N⋅m (72 lbf⋅ft). Flex-Fuel, gasoline (E22) or ethanol (E100). Compression ratio of 11
Nissan_HR_engine
Large twin-aisle airliner family
proposing a 102,000 lbf (454 kN) GE90-102B, while P&W offered its 98,000 lbf (436 kN) PW4098, and Rolls-Royce was proposing a 98,000 lbf (437 kN) Trent 8100
Boeing_777
Afterburning turbofan aircraft engine
used on the F-22 Raptor, the F135 produces around 28,000 lbf (125 kN) of thrust and 43,000 lbf (191 kN) with afterburner. The F135 competed with the General
Pratt_&_Whitney_F135
1990s British turbofan aircraft engine
in) fan and a Trent 800 core scaled down. It produces up to 275 kN (62,000 lbf) of thrust at take-off and has a bypass ratio up to 8.5:1 in cruise. In 1995
Rolls-Royce_Trent_500
1960s British turbofan aircraft engine
made by Rolls-Royce. The engines are capable of generating 41,030 to 59,450 lbf (182.5 to 264.4 kN) of thrust. The RB211 engine was the first production
Rolls-Royce_RB211
Turbojet engine
convergent/divergent exhaust nozzle. The maximum sea-level thrust was 28,800 lbf (128 kN). The YJ93 started life as the General Electric J79-X275, an enlarged
General_Electric_YJ93
Aircraft engine
600 lbf (73.8 kN) in intermediate power and 28,200 lbf (125.4 kN) in afterburner; the figures for the -400, used on the F-14B/D, were 16,333 lbf (72.7 kN)
General_Electric_F110
Unit conversion factor in physics
{\displaystyle F=Kma} If F = 1 lbf, m = 1 lb, and a = 32.174 ft/s2, then 1 lbf = K ⋅ 1 lb ⋅ 32.174 ft s 2 {\displaystyle 1~{\text{lbf}}=K\cdot 1~{\text{lb}}\cdot
Gc_(engineering)
Rocket engine in SpaceX Falcon launch vehicles
launch vehicles, capable of producing 380 kN (85,000 lbf) of thrust at sea level and 420 kN (95,000 lbf) in vacuum, and performing with a specific impulse
SpaceX_Merlin
Soviet high-bypass turbofan
The Progress D-18T (or Lotarev D-18T) is a 51,500 lbf (229 kN) high-bypass turbofan that powers the Antonov An-124 Ruslan and An-225 large freighters
Progress_D-18T
Rocket engine used on the Saturn V rocket
789 kg) of liquid oxygen and 1,738 lb (788 kg) of RP-1, generating 1,500,000 lbf (6.7 MN; 680 tf) of thrust. This equated to a flow rate of 671.4 US gal (2
Rocketdyne_F-1
Turbofan aircraft engine family
F412 are a family of afterburning turbofan engines in the 10,500–19,000 lbf (47–85 kN) class (static thrust). The series is produced by GE Aerospace
General_Electric_F404
Turbojet engine
000 lbf (13 kN) J34-WE-15 3,000 lbf (13 kN), with short afterburner, similar to -42 J34-WE-15 4,100 lbf (18 kN) J34-WE-17 3,370 lbf (15.0 kN) / 4,850 lbf
Westinghouse_J34
Canadian series of aircraft engines
to 3,000 lbf (4.0 to 13.3 kN) of thrust and powering the Eclipse 500/550, the Cessna Citation Mustang and the Embraer Phenom 100. The 2,500 lbf (11 kN)
Pratt_&_Whitney_Canada_PW600
Reciprocating internal combustion engine
for the automatic. The engine produces 69–73 kW (93–98 hp) and 121 N⋅m (89 lbf⋅ft) of torque. The Perodua Bezza Advance variant and all variants of the
Toyota_NR_engine
Aircraft turbofan jet engine
low pressure turbine. It is generally designed to be in the 4,700 to 8,000 lbf (21 to 36 kN) thrust class. The first variant, the PW305A, has the following
Pratt_&_Whitney_Canada_PW300
Measurement unit for pressure
typically between 6 and 7 inches WC or about 0.25 lbf/in2. 1 inAq ≈ 0.036 lbf/in2, or 27.7 inAq ≈ 1 lbf/in2. Pressure head Barometer Millimetre of mercury
Inch_of_water
2010s Russian turbofan aircraft engine
twin-jet airliner. Previously known as the PS-12, it is a 14 tf (30,865 lbf) thrust powerplant that allegedly features many new technologies. The goal
Aviadvigatel_PD-14
Family of internal combustion engines
110 lbf⋅ft) at 2800 rpm. The common (1993 to 1995 North American) version is rated at 82 kW (110 hp; 112 PS) at 5600 rpm and 15.9 kg⋅m (156 N⋅m; 115 lbf⋅ft)
Toyota_A_engine
American low-bypass turbofan engine for the F-22 Raptor
the Lockheed Martin F-22 Raptor. The engine delivers thrust in the 35,000 lbf (156 kN) class and was designed for sustained supersonic flight without afterburners
Pratt_&_Whitney_F119
Franco–American turbofan aircraft engine
made by CFM International (CFMI), with a thrust range of 18,500 to 34,000 lbf (82 to 150 kN). CFMI is a 50–50 joint-owned company of Safran Aircraft Engines
CFM_International_CFM56
Family of jet engines
and produces between 1,000 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
Williams_FJ33
Toyota 4-cylinder engine introduced in 2008
at 5800 rpm, 247 N⋅m (182 lbf⋅ft) at 4200 rpm Toyota Highlander ASU40, 190 PS (140 kW; 187 hp) at 5800 rpm, 252 N⋅m (186 lbf⋅ft) at 4100 rpm Toyota Highlander
Toyota_AR_engine
Turbojet engine for missiles, target drones, and UAVs
vehicles. Variants of this engine produce from 3.5 to 5.3 kN (790 to 1,190 lbf) of thrust. The engine first ran in 1974. The TRI 60 engine was developed
Microturbo_TRI_60
Test to measure resistance of wood
measurement is of balsa, and the softest quipo measured was 46 lbf tangential, 38 lbf radial. Janka Hardness Scale For Wood – Side Hardness Chart of Some
Janka_hardness_test
Afterburning turbofan engine that powers the F-15 Eagle and F-16 Fighting Falcon
continuous power rating of 12,410 lbf (55.2 kN), military power of 14,690 lbf (65.3 kN), and afterburning thrust of 23,930 lbf (106.4 kN) with 5-minute limit
Pratt_&_Whitney_F100
Reciprocating internal combustion engine
256 bhp) at 6,000 rpm; 350 N⋅m (258 lbf⋅ft) at 3,250 rpm — AQG, AKC 206 kW (280 PS; 276 bhp) at 6,000 rpm; 360 N⋅m (266 lbf⋅ft) at 3,750 rpm — BFL applications
Volkswagen-Audi_V8_engine
Turbojet aircraft engine
engine originally designed for the United States Navy, in the 40 kN (9,000 lbf) class. It powered the A-6 Intruder and the AGM-28 Hound Dog cruise missile
Pratt_&_Whitney_J52
Axial flow turbojet engine
given in Pound-force (lbf) and kilonewtons (kN). XJ79-GE-1 Prototype. First ground static test run on 8 June 1954 produced 14,350 lbf (64 kN) with afterburner
General_Electric_J79
Reciprocating internal combustion engine
800-6,000 rpm; 200 N⋅m (148 lbf⋅ft) at 1,500-3,500 rpm — CPWA 90 kW (122 PS; 121 bhp) at 5,000-6,000 rpm; 200 N⋅m (148 lbf⋅ft) at 1,400-4,000 rpm —CMBA
Volkswagen_EA211_engine
1980s Soviet/Russian turbofan aircraft engine
model Tupolev Tu-144LL supersonic transport. It produces 245 kN (55,000 lbf) of thrust in afterburner. An upgraded variant known as NK-32 Tier 2 will
Kuznetsov_NK-32
Rocket engine
propellants to generate a maximum thrust of 6,000 lbf (27 kN). Each of the four combustion chambers produced 1,500 lbf (6.7 kN) of thrust. The engine was not throttleable
Reaction_Motors_XLR11
British rifle cartridge
500 ft/s (760 m/s) with muzzle energies of 4,090 ft⋅lbf (5,550 J),4,200 ft⋅lbf (5,700 J) and 4,160 ft⋅lbf (5,640 J) respectively. The cartridge is appropriate
.375_H&H_Magnum
Turbojet aircraft engine series
800 lbf (12 kN) thrust CJ69-1025 1,025 lbf (4.56 kN) CJ69-1400 1,400 lbf (6.2 kN) lb thrust Model 352 Model 352A Model 352-5a (CJ69-T-1025) 1,025 lbf (4
Teledyne_CAE_J69
1990s British turbofan aircraft engine
(247 cm) fan for a 5:1 bypass ratio, it produces 300.3–316.3 kN (67,500–71,100 lbf) of thrust and reaches an overall pressure ratio of 36:1. It competes with
Rolls-Royce_Trent_700
Proposed aircraft to fill the middle of the market segment
widebodies it would have replaced. It would have been powered by a new 50,000 lbf (220 kN) turbofan from GE Aviation/CFM International or Pratt & Whitney,
Boeing_New_Midsize_Airplane
Revolver cartridge designed by Smith & Wesson (S&W)
can achieve 2,826 ft⋅lbf (3,832 J) of energy by driving a 300 grain .452 caliber bullet at 2,060 ft/s (630 m/s) and 2,885 ft⋅lbf (3,912 J) of energy by
.460_S&W_Magnum
Sino-Tibetan language spoken in India and Tibet
China (1977) Language family Sino-Tibetan Tibeto-Kanauri ? West Himalayish Lahaulic Tinani Language codes ISO 639-3 lbf Glottolog tina1246 ELP Tinani
Tinani_language
1950s British turbojet aircraft engine
900 lbf (8.45 kN). ASV.7 ASV.7/R ASV.7 with re-heat; 2,470 lbf (10.99 kN). ASV.8 (became Viper 8 and Mk.102); Long-life version rated at 1,750 lbf (7.78 kN)
Armstrong_Siddeley_Viper
Executive car
(369 lbf⋅ft) of torque and the EQ Boost starter-alternator delivers additional short-term output and torque of 16 kW (21 hp) and 250 N⋅m (184 lbf⋅ft),
Mercedes-AMG_GT_4-Door_Coupé
Turbojet aircraft engine
vanished. Thrust given in foot-pounds (lbf) and kilonewtons (kN). J65-W-1 7,200 lbf (32 kN) J65-W-2 7,220 lbf (32.1 kN), similar to -1, United States
Wright_J65
Finnish rifle cartridge
16.2-gram (250 gr) bullets, which corresponds to about 6,525 J (4,813 ft⋅lbf) of muzzle energy. British military issue overpressure .338 Lapua Magnum
.338_Lapua_Magnum
High-performance luxury cars brand by BMW
462 N⋅m (341 ft⋅lbf) at 3,000 rpm. In 1981, Alpina introduced the B7 S Turbo with 243 kW (330 PS; 326 bhp) at 5,800 rpm and 500 N⋅m (369 ft⋅lbf) at 3,000 rpm
Alpina
Reciprocating internal combustion engine
39 in × 2.76 in) Reference output: 84 PS (62 kW), 13.8 kg⋅m (135 N⋅m; 100 lbf⋅ft) (gross figures, apply to both 1Y and 1Y-J) Applications: Toyota HiAce
Toyota_Y_engine
1940s British turbojet aircraft engine
125 lbf (22.80 kN) Ghost 53 Mk 1 (105) Ghost 103 rated at 4,850 lbf (21.6 kN) Ghost 104 rated at 4,950 lbf (22.0 kN) Ghost 105 rated at 5,150 lbf (22
De_Havilland_Ghost
Subcompact luxury crossover SUV produced by Audi
4-cylinder 2.0 TDI engine rated at 204 PS (150 kW; 201 hp) and 400 N⋅m (295.02 lbf⋅ft), diesel particulate filter and Bluetec emission control system, quattro
Audi_Q3
Soviet turbofan engine
534 lbf) each. D-436T3 The "T3" variant added a booster section behind the new wide-chord fan and had a maximum thrust around 93 kN (21,000 lbf). The
Progress_D-436
Type of motorcycle
@ 15,250 rpm and 116 N⋅m (86 lbf⋅ft) of torque at 11,750 rpm or 174 kW (233 hp; 237 PS) @ 15,500 rpm and 119 N⋅m (88 lbf⋅ft) of torque at 11,750 rpm with
Ducati_Panigale_V4
Reciprocating internal combustion engine
775 ft⋅lbf (1,051 N⋅m) @ 1200 rpm; 253 horsepower governed at 2100 rpm 816 ft⋅lbf (1,106 N⋅m) @ 1200 rpm; 277 horsepower governed at 2100 rpm 957 ft⋅lbf (1
Detroit_Diesel_Series_92
1960s Soviet turbofan aircraft engine
(20,000 lbf) thrust class. It powered production models of the Ilyushin Il-62 and the Tupolev Tu-154A and B models. NK-8-2 93.2 kN (20,950 lbf) (Tupolev
Kuznetsov_NK-8
1990s Russian turbofan aircraft engine
Russian high-bypass commercial turbofan rated at 16000 kgf (157 kN, 35,300 lbf) thrust. It powers Russian airliners such as the Ilyushin Il-96 and the Tupolev
Aviadvigatel_PS-90
Turning force around an axis
conversion factor 33,000 ft⋅lbf/min per horsepower: power = torque ⋅ 2 π ⋅ rotational speed ⋅ ft ⋅ lbf min ⋅ horsepower 33 , 000 ⋅ ft ⋅ lbf min ≈ torque ⋅ RPM
Torque
Turbofan aircraft engine family
General Motors) and Rolls-Royce plc began joint studies of a 33 kN (7,400 lbf) RB580 to power the proposed Short Brothers FJX regional jet, combining the
Rolls-Royce_AE_3007
Turbofan engine produced by Rolls-Royce beginning 1993
000 to 85,000 lbf (330 to 380 kN), to be certified in early 1995 for a mid-1995 introduction, with growth potential to 90,000–95,000 lbf (400–420 kN) with
Rolls-Royce_Trent_800
1957 turbojet aircraft engine family by Bristol Siddeley
at 6,810 lbf (30.29 kN) dry and 8,170 lbf (36.34 kN) with afterburning. Mk.100 Derated to 4,230 lbf (18.82 kN) Mk.101 Mk.701 Rated at 4,520 lbf (20.11 kN)
Bristol_Siddeley_Orpheus
1940s British turbojet aircraft engine
rather than a scaled-up Rolls-Royce Derwent, with a design target of 5,000 lbf (22 kN), making it the most powerful engine of its era. First run in 1944
Rolls-Royce_Nene
British rimless rifle cartridge
702 ft⋅lbf) . The current standard using smokeless powder is a 26 g (400 gr) bullet at 730 m/s (2,400 ft/s), generating 6,935 J (5,115 ft⋅lbf). This is
.416_Rigby
Turbojet engine for missiles and UAVs
missiles and small unmanned aerial vehicles in the 2.2 - 3.6 kN (500 - 800 lbf) thrust class. The TRI-40 engine is a modified version of the Microturbo
Microturbo_TRI-40
Reconnaissance bomber proposal by Boeing
8,500 lbf (38 kN) or 9,700 lbf (43 kN) with afterburner. Thus 4 × 8500 lbf = 34,000 lbf (150 kN) using that engine, as compared to 6 × 5,200 lbf = 31,200 lbf
Boeing_XB-56
Rifle cartridge
400 gr (26 g) with a muzzle velocity of 2,150 ft/s (660 m/s) and 4,100 ft⋅lbf (5,600 N⋅m) of energy. It is very effective on large game and is favored
.404_Jeffery
Anti-materiel rifle
200 ft⋅lbf (16,500 J) of kinetic energy. The .600 Nitro Express, the second most powerful African big-game rifle cartridge, has around 8,200 ft⋅lbf (11,100 J)
Anzio_20mm_rifle
Turbojet Aircraft Engine
500 lbf (33 kN) thrust at sea level static conditions without afterburner and 10,900 lbf thrust with afterburner. A more powerful model 9,500/13,700 lbf thrust
Westinghouse_J40
Single-person lightweight aircraft
more powerful WR19-9 BRP5, rated at 670 lbf (2.98 kN) thrust and a specific fuel consumption of 0.47 lb/lbf·h (13.31 g/kN·s). U.S. patent 4,447,024 was
Williams_X-Jet
LBF
LBF
LBF
LBF
Boy/Male
Gujarati, Hindu, Indian, Jain, Malayalam, Sindhi, Tamil
Winner; Victory
Girl/Female
Indian, Tamil
Kind-hearted
Boy/Male
Indian, Punjabi, Sikh
Jewel of Virtues
Girl/Female
Hindu, Indian, Marathi, Sanskrit
Lakshmi who is as Graceful as an Elephant
Boy/Male
Indian
Servant of the subduer, The almighty
Girl/Female
Hindu, Indian, Tamil
Divine Power; Lovely
Male
Russian
(ИÑай) Russian form of Greek Esaias, ISAI means "God is salvation."
Surname or Lastname
English
English : habitational name from any of numerous places named with Old English hÄlig ‘holy’ + well(a) ‘well’, ‘spring’, such as Holwell in Dorset and Oxfordshire. (Reaney suggests it could also have been a topographic name with the same etymological origin.) However, the present-day concentration of the name in Northamptonshire would suggest that Holwell in Leicestershire, which has a different etymology, from Old English hol ‘hollow’ + wella, was most likely the primary source of this form of the surname. There is also a Holwell in Hertfordshire of the same derivation, as well as places called Halwill and Halwell in Devon, Holywell in Cambridgeshire, Cornwall, Clwyd, and Northumberland, and Halliwell near Manchester, all of which could have contributed to the surname.
Boy/Male
English
Lives in Wolfe's cottage.
Boy/Male
Hindu
Angel of God on earth, King of the earth
LBF
LBF
LBF
LBF
LBF