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rate and exit pressure pexit

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13y ago

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What are two thrust factors that a rocket engine depends on?

•Thrust depends on two factors: -rate at which momentum leaves the rocket through the nozzle -Exit pressure pexit


The thrust of any rocket engine depends on two factors what are they?

The thrust of a rocket engine depends on the mass flow rate of the propellant and the exhaust velocity of the gases expelled. The mass flow rate is the amount of propellant being burned and expelled per unit time, while the exhaust velocity is how fast the gases leave the engine. Together, these factors determine the overall thrust produced by the engine according to Newton's third law of motion.


What two elements make rocket fuel?

Two common elements found in rocket fuel are liquid oxygen (O2) and liquid hydrogen (H2). When these two elements are combined and ignited in the rocket engine, they react to produce a powerful thrust that propels the rocket into space.


Name the two forces acting on the rocket immediately after leaving the launching pad?

name the two forces acting on the rocket immediately after leaving the launching pad


In a rocket what is an engine mount?

In a model rocket that uses engines, there is an engine mount. The engine mount is located inside the body tube in the bottom where the engine goes. It usually consists of a small tube, two rings that connect it to the body tube, and a metal bar to hold the engine in the tube. Its job is to house the engine and hold it in place for a flight. glad to help, Uujjee


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One of the key factors in rocketry is the weight of the rocket. By designing a rocket that ejects parts of the rocket that has emptied it's fuel tanks decreases the overall weght of the rocket, extending the flight of the rocket.


How many cc is an 10 horse motor?

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What is an ionization engine?

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How long to fly across Russia?

Depends on your means of transportation. If you fly with a rocket, then one or two minutes.


What two factors should you keep in mind when designing and building a rocket?

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Why does a rocket require a rocket engine not a jet engine?

While they may appear to be the same type engine, a jet engine and rocket engine are two separate types of engines. A jet engine functions by pushing air backwards through the use of different methods (turbines, atmospheric pressure, etc.) while a rocket engine operates through the force of its exhaust pushing backwards, thus providing thrust in the opposite direction. In short, because a rocket engine pushes force backwards through its own exhaust, it is more efficient than a jet engine in lower atmospheric pressures or sometimes vacuums (such as in space) A jet, on the other hand, needs air. This is because it uses air as its medium of force and not its own exhaust. In relation to your question, a rocket uses a rocket engine because it is usually built for higher altitudes or escape from the earth's immediate influence altogether. It therefore has more need for an engine to match. They are also used by enthusiasts because they are easier, cheaper (depending on type) and (in comparison, but also depends on type) smaller to build. I hope this answers your question (but probably confused you more) Hopefully, someone else who understands this will simplify it for me, and correct possible mistakes.


How many cams in a v8 engine?

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