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What else can I help you with?
What is the temperature inside the rocket thrust chamber?
more then 190 degrees.that is hot.
What is the simplest engine that is made of a burning chamber and a nozzle?
rocket engine seems to be of this type. as the air-fuel mixture is burned and flame is made to propogate through nozzle to provide thrust
What does the engine do on a space rocket?
Provide thrust ... which changes velocity.
How many forces acting are on a water rocket?
There are two forces acting on a water rocket. The thrust which the force that is given to the water rocket to make it move, and the other one is the gravity.
A rocket will move upward as long as the thrust is greater than the force of gravity?
Actually for some time even after the thrust is no longer greater than gravity. When the rocket's thrust is greater than gravity, it will be accelerating (its velocity upwards will increase). When the rocket's thrust is no longer greater than gravity, at that moment it will still have an upward velocity, so it will still travel upwards - it will only travel more and more slowly upwards as gravity starts to sap the rocket's upward velocity towards zero. Once its velocity reaches zero, if gravity is still winning over the rocket's thrust (if any), then it will start to fall back towards the ground.We are assuming a simplistic model (no air resistance, no super-unlucky collisions with meteors, etc.), but this is the basic idea.
What is the upper chamber of the nozzle of a rocket?
Thrust Chamber
What is the temperature inside the rocket thrust chamber?
more then 190 degrees.that is hot.
How does a rocket create lift?
thrust. thrust is how a rocket creates lift. thrust is simply the difference in potential energy between the nozzle and the combustion chamber, the difference creates a pressure differential which causes the rocket to move. To go up the rocket must be perfectly balanced and the rocket frame must be strong enough to withstand and balance the thrust.
What is a rocket and how it works?
A rocket is a vehicle that uses propellants to generate thrust for propulsion. The propellants are ignited in a combustion chamber, creating a high-pressure gas that is expelled through a nozzle at the rear of the rocket. This action creates a reaction force known as thrust, propelling the rocket forward.
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.
How could a toy rocket accelerate after takeoff?
As long as the thrust is more than the weight of the rocket (toy or otherwise) the rocket will accelerate. When the thrust matches the weight, the rocket will cruise. When the thrust is less then the rocket will slow.
How does the liquid fuel rocket work?
by burning liquid fuel with a liquid oxidizer in a combustion chamber connected to the exhaust nozzle. this generates thrust.
During a rocket launch whioch is greater thrust of the rocket engine or weight of the rocket?
During a rocket launch, the thrust of the rocket engine is greater than the weight of the rocket. This is necessary for the rocket to overcome Earth's gravitational pull and lift off into space. The thrust generated pushes the rocket upwards while gravity pulls it down.
A rocket uses an engine that creates thrust through the combustion of a liquid fuel and ain oxidizer?
Yes, that's correct. Liquid fuel and an oxidizer are burned in the rocket engine's combustion chamber to create high-pressure exhaust gases that are expelled out of the nozzle at high speed, generating thrust that propels the rocket forward.
How many pounds of thrust did the rocket achieve on liftoff?
The thrust of a rocket on liftoff can vary depending on the rocket's design and size. For example, the Falcon 9 rocket produces about 1.7 million pounds of thrust at liftoff.
What is a device that is driven forward by a powerful stream of hot gas?
A Rocket
What has the author Douglas C Rapp written?
Douglas C. Rapp has written: 'Reliability assessment of thrust chamber cooling concepts using probabilistic analysis techniques' -- subject(s): Thrust, Monte Carlo method, Rocket engines 'High energy-density liquid rocket fuel performance' -- subject(s): Liquid propellants, Rocket engines
