there, In accordance with the question :
It depends on how big the exhaust or the outlet hole is from the cylinder. The bigger the hole, the lower the thrust. But it doesnt mean that the hole should be extremely small. Its correct size deliver max thrust.
The highest temperature warning is because as gasses heat they expand and take up more space. If a container gets too hot the gasses reach a point where their volume is too much for the container and the metal can not longer retain its shape, thus causing the cylinder to burst (typically very violently).
Air is much easier to compress compared to water because air is a compressible gas, while water is an incompressible liquid. This means that when pressure is applied, air molecules can be compressed closer together, whereas water molecules are already closely packed and cannot be compressed to the same extent.
An XL50 oxygen cylinder weighs approximately 16 pounds when full.
A standard oxygen cylinder contains around 6,000 liters of oxygen when full.
If air is compressed and cooled, the temperature of the air will become negative. Now depending on how much humidity there is in that air being compressed we might get some water droplets as it is being cooled. Carbon dioxide when compressed and cooled we get dry ice.
Depends on the size of the cylinder, if the air is compressed or not and if it is compressed, to how much psi.
The thrust generated by a solid fuel rocket varies widely depending on its design, size, and the specific type of propellant used. Typically, solid rocket motors can produce thrust ranging from a few thousand pounds to several million pounds. For example, the Space Shuttle's Solid Rocket Boosters generated about 2.7 million pounds of thrust each at launch. The thrust can be calculated using the formula ( F = \dot{m} \cdot v_e ), where ( F ) is thrust, ( \dot{m} ) is the mass flow rate of the propellant, and ( v_e ) is the effective exhaust velocity.
"Force the substance into a smaller volume" is pretty much the definition of "compress".
The Concorde's engines, specifically the Rolls-Royce/Snecma Olympus 593 engines, each produced approximately 38,050 pounds of thrust at takeoff. With four engines, the total thrust generated was around 152,200 pounds. This powerful thrust allowed the Concorde to reach supersonic speeds and maintain its unique cruising altitude.
Whatever amount of pressure was used to compress the CO2 originally, can be reached (or nearly reached) when it is released into an air cylinder.
Thrust Capacity is how much thrust it can take :D
about 7.2 million pounds of thrust (Solid Rocket Boosters and Main Engines combined)
A Boeing 747 typically has four engines, and each engine produces approximately 66,500 to 70,000 pounds of thrust, depending on the specific model and engine type. This means the total thrust generated by all four engines can range from about 266,000 to 280,000 pounds. The high thrust allows the aircraft to efficiently take off and climb at high altitudes.
Every year the mountain grows taller by 4mm as a result of the upward thrust generated by two opposing tectonic plates.
The thrust generated in a solid fuel rocket engine is primarily determined by the type and composition of the propellant, the design of the combustion chamber, and the nozzle configuration. The burn rate of the solid fuel, which can be influenced by factors such as temperature and pressure, also plays a crucial role. Additionally, the nozzle shape affects how efficiently the exhaust gases are expelled, impacting the thrust produced. Ultimately, these factors interact to determine the overall performance of the rocket engine.
A Saturn V rocket could produce up to 7.5 million pounds of thrust at liftoff, making it one of the most powerful rockets ever built. This immense thrust was generated by the five massive F-1 engines in the first stage of the rocket.
The amount of thrust depends on the power of the engine