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What is the reason for having a combustion chamber on a rocket?
A combustion chamber is where combustion occurs in a controlled fashion. Because the basic idea of a rocket is burning fuels and directing them in the opposite direction to that of travel, a controlled burning - as happens in the combustion chamber - is exactly what a rocket needs to work.
What is the process of single stage rocket?
combustion
What is the process of a single stage rocket?
combustion
A rocket uses an engine that creates thrust throughout the combustion of a liquid fuel and an oxidizer what kind of rocket is this?
Chemical rocket
A rocket uses an engine that creates thrust through the combustion of a liquid fuel and an oxidizer. What kind of rocket is this?
Chemical rocket
What happens when gas molecules hit the inside of a rocket's combustion chamber?
The rocket pushes back on the gas.
What happens when gas molecules hit inside of the rocket's combustion chamber?
The rocket pushes back on the gas.
What causes the forward motion of a rocket?
The forward motion of a rocket is caused by the expulsion of high-speed exhaust gases from the combustion of rocket fuel. Newton's third law of motion states that for every action, there is an equal and opposite reaction, so the force of the expelled gases propels the rocket forward.
When combustion reactions occur inside a rocket's engine a lot of heat and pressure are released The pressure gradient is much larger inside the rocket than outside which causes the?
thrust
What is the combustion chamber of a rocket?
The combustion chamber of a rocket is the part of the engine where fuel and oxidizer are mixed and burned to produce hot, high-pressure gas that is expelled through the nozzle to create thrust. It is a critical component that helps propel the rocket into space.
Where do the rocket exerts force in pressure?
Rockets exert force at the upper part of the combustion chamber. This pushes the rocket forward.
How does a rocket moves forward?
Rockets are propelled forward by thrust generated by the combustion of rocket fuel and controlling the direction of the exhaust.
