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500 hp (370 | kW) steel tug. |
720 hp (537 | kW) projected - Fully supercharged |
F.22 - 260 hp (194 | kW) Sunbeam Maori II |
Powered by 80 hp (60 | kW) Gnome engine. |
Single aircraft powered by 70 hp (50 | kW) Daimler engine. |
Engine type: 500 hp (370 | kW) V8 Detroit Diesel (8V92) |
Powered by 200 hp (149 | kW) Hispano-Suiza engine. |
Revised version with 130 hp (97 | kW) Clerget 9C engine. |
Other engines used include the 50 hp (37 | kW) Rotax 503 and 45 hp (34 kW) Zanzottera MZ 201. |
The 1489 cc engine produced 68 hp (51 | kW) at first, but was soon uprated to 72 hp (54 kW) |
Output was 81 hp (60 | kW), a figure that was increased to 90 hp (67 kW) i |
arines, U-64 had a total output of 1,000 hp (746 | kW) while submerged and 4,400 hp (3,281 kW) when su |
o articles: XPG-2 engines changed to 200 hp (150 | kW) plus one CG-4A converted also with 200 hp (150 |
plications raised maximum power from 165 hp (123 | kW) to 175 hp (130 kW), but more significantly rais |
The 322 hp (240 | kW) was the only output for 1959, and power dropped |
The second, powered by an Eagle V of 275 hp (205 | kW), was designated F.17. |
It is powered by a 160 hp (120 | kW) Lycoming O320D engine. |
This model has a one-cylinder 5 hp (3.7 | kW) air-cooled engine. |
At wheels with consist: 2,950 hp (2,200 | kW) while providing HEP for 12 MLV consist |
Powered by two 1,460 hp (1,089 | kW) Roll-Royce Merlin 31 piston engines. |
250 hp (186 | kW) was on tap, and 6 or 7 were made. |
Nos. 7927 and 8524, GE 380 hp (280 | kW) built 1944 |
It had a 1,100 hp (820 | kW) generator and serviced 107 consumers by 1905. |
For power, it employed a pair of 90 hp (67 | kW) Curtiss OXX-2s, between the wings. |
of the 20 Y1C-14s re-engined with a 575 hp (429 | kW) Wright R-1820-7 Cyclone. |
Civil production version with a 525 hp (391 | kW) Wright R-1750-3 radial engine. |
rd Mk I - Prototype - powered by two 320 hp (239 | kW) ABC Dragonfly engines - one built. |
Single-seat bomber powered by a 200 hp (149 | kW) Hispano-Suiza 8 engine. |
e initial version was powered by two 450 hp (340 | kW) Lorraine-Dietrich broad arrow engines. |
It produced 20 hp (15 | kW) for a top speed of 45 mph (72 km/h). |
1999/2001 Ford Mustang SVT Cobra, 320 hp (239 | kW) and 317 lb·ft (430 N·m) |
It produced 150 hp (112 | kW) and was an unusual 65° L-head design. |
Two 100 hp (75 | kW) Sunbeam or 75 hp (56 kW) Rolls-Royce Hawk engin |
these units are usually rated at 4,000 hp (3,000 | kW) instead of the usual 4,400 hp (3,300 kW) offere |
he first and third were powered by a 200 hp (150 | kW) Hispano-Suiza and the second by the 150 hp (110 |
U, one other initially had a 220 PS (217 hp, 162 | kW)Argus As17B inline engine and later a 160 PS (15 |
The output is 110 hp (82 | kW) at 3,000 rpm, 130 hp, 160 hp, 190 hp, 220 hp (1 |
ed as a larger engine to replace the 300 hp (224 | kW) gasoline engines, this new V8 design produces 3 |
was a 6-cylinder petrol engine with a 90 hp (67 | kW) generator driving two 60 hp (45 kW) electric mo |
Output ranged from 130 hp (97 | kW) with the B30A equipped with two Zenith-Stromber |
ratt & Whitney XR-1340-43 engines of 550 hp (410 | kW) each compared to the two Pratt & Whitney R-985- |
car offering fewer appointments and 228 hp (170 | kW), as well as the standard turbo still offering 2 |
production Tipsy S.2s used either the 32 hp (24 | kW) Sarolea Epervier (eng: Sparrowhawk) in Belgian- |
e the expected power, producing only 200 hp (149 | kW) instead of the expected 260 hp (194 kW). |
ith a displacement of 633 cc producing 19 hp (14 | kW) and later 767 cc, yielding 21.5 hp (16 kW) at 4 |
igh wing light aircraft powered by a 225 hp (168 | kW) Continental O-470-A, O-470-J, or a 230 hp (172 |
Power was from a 200 hp (149 | kW) Rolls-Royce Falcon engine with radiators on eac |
Output is 192 hp (143 | kW) at 6000 rpm with 181 ft·lbf (245 Nm) of torque |
nd, 1930 saw the company introduce the 37 hp (28 | kW) A-40 four-cylinder engine. |
my based on the 47G-3B-1, powered by 270 hp (201 | kW) Lycoming TVO-435-D1B. |
gined three-bay biplane powered by a 250 hp (186 | kW) Rolls-Royce engine. |
were converted, and fitted with the 785 hp (585 | kW) Hispano-Suiza 12Xbrs engine. |
Model C, patented in 1911, 4 hp (3.0 | kW) engine most commonly known for driving oat bind |
-speed version, powered by a 400 PS (395 hp, 294 | kW) Hirth HM 512 engine. |
e reliable engine was tested, but the 120 hp (90 | kW) Beardmore did not help meet the performance req |
l compound expansion steam engine of 850 hp (634 | kW) driving a single screw. |
r, four stroke engine of 933 cc giving 21 hp (16 | kW) at 3400 rpm. |
TKF - TK tankette with 46 hp (34 | kW) Polski Fiat engine and new (TKS-type) suspensio |
Traction was provided by two fixed 54 hp (40 | kW) steam engines, though only one was used in norm |
elopment of the F.2a, powered by two 320 hp (239 | kW) Sunbeam Cossack engines. |
e direct injected engines ranging from 15 hp (11 | kW) to a 3.4L V6 300 hp. |
e placed for aircraft powered by the 230 hp (170 | kW) BHP Puma, 400 hp (300 kW) Fiat, 400 hp (300 kW) |
263 hp (196 | kW) at 6250 rpm and 249 lb·ft (338 N·m) at 4500 rpm |
Ti-VCT 305 hp (227 | kW) at 6500 rpm and 280 lb·ft (380 N·m) at 4250 rpm |
262 hp (195 | kW) at 6250 rpm and 248 lb·ft (336 N·m) at 4500 rpm |
It will have an estimated 950 hp (708 | kW) and an estimated top speed of 254 mph (409 km/h |
aissance, training model, powered by a 70 hp (52 | kW) Gnome 7B rotary piston engine. |
with 250 cm3 (15 cu in) displacement, 55 hp (41 | kW) a weight of 27.8 kg (61 lb). |
It was powered by a nose-mounted 100 hp (75 | kW) Gnome Monosoupape rotary engine driving a two-b |
The powertrain was rated at 164 hp (122 | kW) and 159 lb·ft (216 N·m) of torque. |
The first car was a 6 hp (4.5 | kW) single-cylinder tiller-steered runabout named t |
r cylinder, four stroke 1172 cc giving 34 hp (25 | kW) at 4250 rpm. |
e-Dietrich engine, the rest with the 760 hp (570 | kW) Hispano-Suiza 12Lb. |
n with fabric skinning, powered by a 200 hp (150 | kW) Hispano-Suiza engine. |
It was powered by a nose-mounted 225 hp (168 | kW) Sunbeam Mohawk engine driving a two-bladed prop |
as a twin-float biplane powered by a 220 hp (164 | kW) Mercedes D.IV engine. |
The 1.7 liter engine produced 80 hp (60 | kW), the 1.8 produced 79, and the 2.0 liter engine |
ineer to run the engine with all 4,400 hp (3,300 | kW) if necessary. |
"Vuia II" airplane, with an Antoinette 25 hp (19 | kW) internal combustion engine, was exhibited at th |
g a single screw with a power of 1,950 hp (1,454 | kW) shaft. |
The Spanish requested the use of the 70 hp (50 | kW) Renault engine which they already used in their |
generator spec has an output of 2,936 hp (2,189 | kW) from a capacity of 2,980 cubic inches (48,800 c |
omebuilt market, powered by a standard 40 hp (30 | kW) Rotax 447 engine, mounted in pusher configurati |
table landing gear, powered by two 1375 hp (1025 | kW) Bristol Hercules radial piston engines. |
id-cooled V-12 engine, producing 2,340 hp (1,745 | kW) and driving two three-bladed contra-rotating pr |
es, designated F.16 and powered by a 250 hp (190 | kW) Rolls-Royce Eagle IV. |
A follow-on design, the 50 hp (37 | kW) A-50 was introduced in 1938 and was used to pow |
r-cylinder, four-stroke 3285 cc giving 50 hp (37 | kW) at 2800 rpm. |
the front of the car was an air-cooled 75 hp (56 | kW) Renault engine driving a 9 ft (2.7 m) diameter |
riolet, which combined the Turbo S's 250 hp (186 | kW) engine with the cabriolet body. |
howed the SOHC Hemi producing almost 700 hp (522 | kW) in crate form (100 hp per liter). |
ompact tractor biplane, powered by a 200 hp (149 | kW) Hispano-Suiza water cooled engine. |
rst flew on 22 June 1917, powered by a 35 hp (26 | kW) ungeared Gnat engine, as the geared engine was |
12.7 cu in) 6-cyl 4-stroke engine with 85 hp (63 | kW) and a top speed of 100 km/h (62 mph). |
) first flew in 1923 powered by four 650 hp (485 | kW) Rolls-Royce Condor IA piston engines. |
The ABC Gnat was a 45 hp (34 | kW) two-cylinder aero engine designed by the noted |
J version was used, pushing power to 140 hp (104 | kW) allowing the car 120 mph (193 km/h). |
y until 7 September 1917, powered by a 35 hp (26 | kW) ungeared Gnat engine, as the originally planned |
by a Griffon 89 engine rated at 2,350 hp (1,752 | kW) driving two three-bladed contra-rotating propel |
The originally planned 1,900 hp (1,400 | kW) DB 603G engine was cancelled in early 1944, so |
ne, another water-cooled radial, the 260 hp (195 | kW) Salmson 9Za. |
s not ready and it was fitted with a 160 hp (120 | kW) Beardmore engine instead. |
as designed to use a new engine, the 230 hp (170 | kW) BHP inline engine (later to become the Siddeley |
connected to two shafts giving 11,000 hp (8,200 | kW), which could propel the ship at 17 kn (20 mph; |
s, serial number N.100, powered by a 200 hp (149 | kW) Sunbeam Arab engine started testing in June 191 |
lets added, low pressure tyres and a 180 hp (134 | kW) Lycoming engine. |
placed the engine with a more powerful 72 hp (54 | kW) Gleniffer diesel engine giving her an extra 2 k |
The engine was a 3160 cc, 4 cylinder, 20 hp (15 | kW) unit, it cost £500 with seven-seated touring co |
red in 1920, as testbeds for the new 150 hp (112 | kW) Armstrong Siddeley Lynx radial. |
(1796cc) version of the M40 producing 115 hp (86 | kW) of mechanical power and 122 ft·lbf (165 N·m). o |
ased on the Thorp T211 with a lighter 120 hp (89 | kW) Jabiru 3300 engine and it is certified as a Lig |
C classification system, generated 1425 hp (1060 | kW), and ran at up to 100 km/h. |
The following year it had a 25 hp (19 | kW) Ava engine, then a variety of small engines inc |
r 200 bombers, to be fitted with 1,600 hp (1,195 | kW) Wright R-2600-A5B Double Cyclone engines. |
nce 4 was a British experimental 2,000 hp (1,490 | kW) class H-24 aircraft engine designed and built b |
Patrol Seaplane, being powered by a 200 hp (149 | kW) Sunbeam engine. |
Output was 120 hp (89 | kW) at 3600 rpm and 205 lb·ft (278 N·m) of torque a |
r based on the F.3, but powered by a 300 hp (224 | kW) Hispano-Suiza engine, the F.4 Buzzard. |
Output is 200 hp (147 | kW) at 6000 rpm with 221 ft·lbf (300 N m) of torque |
e second prototype was fitted with a 360 hp (267 | kW) ABC Dragonfly radial engine, becoming the Bulld |
g more improvements, including a 1,350 hp (1,010 | kW) engine, but production ended in summer 1944; 45 |
swagen versions originally featured an 80 hp (60 | kW) fuel-injected 1.7 L flat-4 engine based on the |
Output (on the MPV) is 200 hp (150 | kW) at 6200 rpm with 200 lb·ft (270 N·m) of torque |
dvance was an English tricar producing 6 hp (4.5 | kW) offered from 1902 to 1912 by a Northampton moto |
(120 cu in) TDI I4 producing around 180 hp (130 | kW) and 260 lb·ft (350 N·m). |
by Wing warping, and was powered by an 80 hp (60 | kW) Gnome Lambda rotary engine. |
A8963 was rebuilt with a 200 hp (149 | kW) Hispano-Suiza engine, and modified wings as the |
1918, a second 530 was fitted with a 200 hp (150 | kW) Sunbeam Arab engine, but development was subseq |
12-cylinder petrol engines generated 630 hp (470 | kW) on each of two shafts for a speed of 20 knots ( |
oyce Falcon III engine replacing the 250 hp (120 | kW) Rolls-Royce Falcon II. |
outh African Air Force, powered by a 480 hp (358 | kW) Bristol Jupiter VIII radial piston engine. |
Drain into the Trent was replaced by a 43 hp (32 | kW) steam-powered beam engine in 1847. |
The 477 produced 260 hp (194 | kW) at 3600 rpm and 430 lb·ft (583 N·m) of torque a |
The 534 produced 277 hp (207 | kW) at 3400 rpm and 490 lb·ft (664 N·m) of torque a |
introduced in 1958, the 401 produced 226 hp (169 | kW) at 3800 rpm and 350 lb·ft (475 N·m) of torque a |
was powered by the Beardmore, or by 150 hp (112 | kW) Hispano-Suiza engines, later aircraft were fitt |
hort S.45, like the S.36, powered by a 70 hp (52 | kW) Gnome, and the larger Short S.41 powered by a 1 |
On the power of its 110 hp (82 | kW) Le Rhone rotary engine it was not outstandingly |
Output was 325 hp (242 | kW) at 3300 rpm and 560 ft·lbf (759 Nm) at 2000 rpm |
entley's Arnage R version to produce 400 hp (300 | kW) and 616 lb·ft (835 N·m) of torque. |
nd 540 long tons (550 t) and her 7,000 hp (5,200 | kW) Parsons turbines and Yarrow boilers produced an |
he opportunity to drive one of their 470 hp (350 | kW) cars, after the rookie had won the ADAC VW Lupo |
rrow water-tube boilers produced 7,000 hp (5,200 | kW) and a top speed of 25.5 kn (29.3 mph; 47.2 km/h |
, being powered by the new Type 209, 300 hp (220 | kW) at 6600 rpm, 4.0 L engine. |
(1.6 L) engine rated from 6.5 to around 9 hp (7 | kW) depending on model. |
ith a more generously powered 3622 cc, 90 hp (67 | kW) sidevalve V8 engine, having a stroke of 92.25 m |
edes-Benz W125 attained an output of 646 hp (475 | kW), a figure not exceeded in Grand Prix Racing unt |
f ventillating traction motors each of 44 hp (33 | kW) were used for a total tractive effort of 6,200 |
With 350 hp (260 | kW), the new 3.0 L air-cooled flat-8 that powered t |
power absorber will provide exactly 200 hp (150 | kW) of load against it, keeping the RPM at 5000 RPM |
was enlarged to 2998 cc (183ci) with 400 hp (298 | kW), which put the 33/3 in the same class as the Po |
to allow fitting of a more powerful (140 hp (104 | kW)) two-row Gnome engine, which was built as the B |
The EMD SW1500 was a 1,500 hp (1,119 | kW) diesel locomotive intended for switching servic |
d with a 3.5 L LX9 V6 that generates 200 hp (149 | kW) and 220 lb·ft (300 N·m) torque, going from 0-60 |
For 2006, a 3.9 L LZ9 V6, with 240 hp (179 | kW) and 240 ft·lbf (332 Nm) torque, was added as an |
f the Bentley turbocharged V8 making 450 hp (340 | kW) and 645 ft·lbf (875 N·m) of torque. |
powerplant was changed again, to the 200 hp (149 | kW) Hispano-Suiza 8 engine, which was mounted at an |
tely working prototype featured a 3L 300 hp (220 | kW) V8 that powered the rear wheels, and underwent |
Its engine was a 160 hp (119 | kW) twin overhead cam evolution of the supercharged |
Rare options: RPO 579E 283 hp (211 | kW) engine (1-hp per cubic inch!) with fresh air/ta |
Tipsy S prototype began flying with an 11 hp (8 | kW) Douglas Sprite, making its first flight on 11 M |
with a broad power curve peaking at 146 hp (109 | kW) near the 10,500 rpm redline. |
ngines, with the right engine producing 10 hp (8 | kW) more power than the left one (the engines are i |
ers and 9 ft (2.7 m) stroke produced 230 hp (170 | kW) and was capable of propelling the vessel at ove |
her Maudslay machinery produced 7,300 hp (5,400 | kW), slightly less than her stablemate HMS Mercury, |
followers (RFF) instead and produced 201 hp (150 | kW) at 5900 rpm with 207 lb·ft (281 N·m) of torque |
compartment in the back, housing the 100 hp (75 | kW) engine (a four-cylinder shortened Ricardo desig |
a four-cylinder watercooled engine of 22 hp (16 | kW), with Gray and Davis generator, optional Gray a |
2004 to 2009 and increased power to 400 hp (298 | kW) and enhanced computer systems decreased the tim |
a 90 cm space between the roof and the 60 hp (45 | kW) engine. |
dern F1 designs which delivered over 400 hp (300 | kW), but were not suited to endurance racing. |
mour plating, powered by two 600 PS (592 hp, 441 | kW) Argus As 411 engines. |
in Heathrow, and was powered by two 460 hp (340 | kW) Bristol Jupiter VIII radial engines. |
The siren was originally powered by a 15 hp (11 | kW) engine, which gave two blasts in quick successi |
Canada offered to supply war-surplus 450 hp (340 | kW) Wasp Jr engines at a low price, the aircraft en |
for the Schneider Trophy, producing 925 hp (690 | kW) at 3300 rpm. |
le-seat parasol monoplane powered by a 30 hp (22 | kW) Carden-Ford converted car engine. |
two-bay tractor biplane powered by a 100 hp (75 | kW) Gnome Monosoupape rotary engine to compete in t |
elage, increased all-up weight and a 145 hp (108 | kW) de Havilland Gipsy Major 7 engine. |
uction automobile engine to attain a 400 hp (298 | kW) advertised rating.This engine featured the trip |
r 100 lb (45 kg) bombs, powered by a 450 hp (336 | kW) Pratt & Whitney R-985-AN2 engine, 1006 built. |
finally brought the engine up to 137.5 hp (102.5 | kW) per cylinder and 406 ft·lbf (550 N·m) torque pe |
ce Griffon 56 engine, delivering 2,000 hp (1,491 | kW) to a 13 ft (4 m), six-blade (two three-bladed p |
e of the bi-turbo 2.7L V6 to produce 480 hp (358 | kW) at 6800 rpm, and 417 ft·lbf (565 N·m) of torque |
ubic inch) P4C engine, producing 45 or 60 hp (45 | kW), was extremely popular in Europe and Israel for |
1689 cm³ (103 in³) engine producing 135 hp (101 | kW) is based on the OM 668 engine from Mercedes-Ben |
roduction batches being powered by a 265 hp (198 | kW) Sunbeam Maori engine owing to shortages of Eagl |
generated an indicated horsepower of 233 hp (174 | kW); driving a single screw, this gave a maximum sp |
eries with a jury rig, with a medium 450 hp (340 | kW) engine for speeds of 5.8 knots (10.7 km/h) to 8 |
Bantam and the Sopwith Snail) by the 170 hp (127 | kW) ABC Wasp radial engine. |
available with the 1.8L Turbo 4 cil 150 hp (112 | kW) with 5 speed Tiptronic automatic gearbox in Com |
ction engine to deliver in excess of 300 hp (224 | kW) and 30 MPG. |
on tractor pulling class, making 8,000 hp (6,000 | kW) at 2,500 rpm. |
d by a 150x100ft electric plant with 150 hp (110 | kW) Corliss steam engine(s) running 500 volt Westin |
gned a number of aircraft to use the 150 hp (112 | kW) Hart radial engine, the development of which wa |
er and heavier, and was powered by a 275 hp (205 | kW) Lorraine Deitrich 8Bd water cooled V-8, with th |
spite the engine only delivering about 82 hp (61 | kW) instead of the promised 100 hp. |
n the Continental R. Power output of 325 hp (242 | kW) and torque of 450 ft·lbf (610 N·m) was estimate |
offered three models, all with Mosher's 12 hp (8 | kW) two-cylinder engine, on the same 84 in (2134 mm |
bocharger and intercooler, producing 325 hp (242 | kW) and 570 lb·ft (773 N·m) with an 18:1 compressio |
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