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In the case of helicopters, tanks are placed on or outside the body of the aircraft, while a spray rig, extending outward to the sides, is attached well below the main rotor blades. Hydroseeding is often done by helicopters using tanks and drop systems much like those used for aerial firefighting .
In the United States, where state sanctioning laws often prohibit inter-divisional bouts, the super heavyweight class is necessary to pair two fighters above 265 lb. Aside from open-weight competitions, the division has never been fully endorsed by any major promotion (except for the open weight bouts of MFC , M-1 , and DREAM ).
100 Pa Pressure due to direct impact of a strong breeze (~28 mph or 45 km/h) [27] [28] [31] 120 Pa Pressure from the weight of a U.S. quarter lying flat [32] [33] 133 Pa 1 torr ≈ 1 mmHg [34] ±200 Pa ~140 dB: Threshold of pain pressure level for sound where prolonged exposure may lead to hearing loss [citation needed] ±300 Pa ±0.043 psi
The Ultimax 100 is a gas-operated automatic weapon (capable of fully automatic fire only) with a short-stroke gas piston operating system powered by ignited powder gases diverted from the barrel through a port in the gas block. The Ultimax 100 is a locked breech weapon with a rotating bolt that contains seven locking
In engineering, the ultimate load [1] is a statistical figure used in calculations, and should (hopefully) never actually occur.. Strength requirements are specified in terms of limit loads (the maximum loads to be expected in service) and ultimate loads (limit loads multiplied by prescribed factors of safety).
It is designed to have either a 100 hp (75 kW) or 180 hp (134 kW) engine fitted for example a 100 hp (75 kW) Continental O-200 engine. [1] It is a braced biplane with wooden wings, a welded steel tube fuselage, fixed conventional landing gear with a tailwheel and a single open cockpit. [ 1 ]
The EMD 265H had a bore of 265 millimetres (10.4 in) and stroke of 300 millimetres (12 in) (so that the displacement per cylinder was 1010 cubic inches) with the 16 cylinder GM16V265H rated at 4,700 kilowatts (6,300 hp) at 1000 rpm, with a brake mean effective pressure of 21.3 bars (2,130 kPa).
When the load factor is +1, all occupants of the aircraft feel that their weight is normal. When the load factor is greater than +1 all occupants feel heavier than usual. For example, in a 2 g maneuver all occupants feel that their weight is twice normal. When the load factor is zero, or very small, all occupants feel weightless.
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