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The Suzuki GSX-R400 was a 400 class sport bike produced by Japanese ... The power-to-weight ratio was increased to 0.39 hp/kg with the new chassis and shorter ...
In a zero-gravity (weightless) environment, the power-to-weight ratio would not be considered infinite. A typical turbocharged V8 diesel engine might have an engine power of 250 kW (340 hp) and a mass of 380 kg (840 lb), [1] giving it a power-to-weight ratio of 0.65 kW/kg (0.40 hp/lb).
Curb weight: 2,093 kg (4,614 lb) ... 276 PS (272 hp; 203 kW) @5000, 400 N⋅m (295 lb⋅ft) @1300–4500 ... 2 strength-to-weight ratio: 6.68. Fourth generation (W167 ...
Despite having larger displacement, it is 17.6 lb (8.0 kg) lighter than the Ninja 300. [1] [4] It has a steel trellis frame with engine as a stressed member resulting in weight reduction of 6 kg (13 lb) and LED headlights and taillights. [7] [6] The engine has a large air-box for intake efficiency along with downdraft air intake.
Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio AJ-10-190 USA: Aerojet: Space Shuttle, Orion, Apollo CSM: Active Upper N 2 O 4 /MMH: Pressure-fed: 316 [1] 26,689 [1] 8.62 [1] 118 [1] 23.08: Archimedes New Zealand USA: Rocket Lab: Neutron: Development 1st, 2nd CH 4 / LOX: Staged, oxidizer-rich ...
The 2020 US model year B58 3.0 L engine was rated at 250 kW (335 hp) and 495 N⋅m (365 lb⋅ft), yet in dynamometer testing by Car and Driver magazine, the 2020 model year Supra had a power output of 257 kW (345 hp) and 555 N⋅m (409 lb⋅ft) at the wheels. Similarly, the 2021 onwards model year engine was rated at 285 kW (382 hp) and 499 N ...
Curb weight: 4,647–4,841 lb (2,108–2,196 kg) ... 2 strength-to-weight ratio: 4.00. Second generation (2018) ... and 295 pound-feet (400 N⋅m) of torque was the ...
The weight (N) is calculated by multiplying the mass in kilograms (kg) by the acceleration due to gravity (m/s 2). The thrust can also be measured in pound-force (lbf), provided the weight is measured in pounds (lb). Division using these two values still gives the numerically correct (dimensionless) thrust-to-weight ratio.