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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.

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What determines how much thrust is generated in a solid fuel rocket engine at?

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.


What are the three types of rocket fuels?

The three types of rocket fuels are liquid rocket fuel, solid rocket fuel, and hybrid rocket fuel. Liquid rocket fuel consists of liquid components that are combined and ignited to produce thrust. Solid rocket fuel is a mixture of solid components that burns to produce thrust. Hybrid rocket fuel combines elements of both liquid and solid rocket fuels.


What determines how much thrust is generated in a solid fuel rocket engine at any given time?

The amount of exposed surface area of the fuel


What controls the thrust of a rocket?

Liquid rocket engines would act much like a car engine. More fuel, more thrust. Solid rocket engines are either on or off. No throttle control.


How many tons of rocket fuel does the shuttle use during liftoff?

The Space Shuttle used approximately 1.6 million pounds (800 tons) of solid rocket fuel during liftoff. This solid rocket fuel was primarily used in the twin solid rocket boosters that provided the initial thrust to launch the shuttle into space.

Related Questions

What determines how much thrust is generated in a solid fuel rocket engine at?

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.


What are the three types of rocket fuels?

The three types of rocket fuels are liquid rocket fuel, solid rocket fuel, and hybrid rocket fuel. Liquid rocket fuel consists of liquid components that are combined and ignited to produce thrust. Solid rocket fuel is a mixture of solid components that burns to produce thrust. Hybrid rocket fuel combines elements of both liquid and solid rocket fuels.


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.


What determines how much thrust is generated in a solid fuel rocket engine at any given time?

The amount of exposed surface area of the fuel


What are the two types of rocket fuel?

The two types of rocket fuel are liquid fuel and solid fuel. Liquid fuel rockets use a combination of liquid propellants, such as liquid oxygen and liquid hydrogen, that are mixed and burned to create thrust. Solid fuel rockets have a solid mixture of fuel and oxidizer that is ignited to produce thrust.


What controls the thrust of a rocket?

Liquid rocket engines would act much like a car engine. More fuel, more thrust. Solid rocket engines are either on or off. No throttle control.


What is Rockets reaction force?

Rocket reaction force, also known as thrust, is the force exerted by a rocket engine to propel the rocket forward. This force is generated by the combustion of fuel in the rocket engine and is directed opposite to the direction in which the rocket travels. The magnitude of the thrust determines the acceleration of the rocket.


What some types of rocket motors?

There are several types of rocket motors, including solid rocket motors, liquid rocket engines, and hybrid rocket engines. Solid rocket motors use a solid propellant that burns uniformly, providing thrust until the fuel is consumed. Liquid rocket engines utilize liquid fuel and oxidizer, allowing for adjustable thrust and the ability to shut down and restart. Hybrid rocket engines combine aspects of both, using a solid fuel and a liquid oxidizer, offering some advantages in performance and safety.


What does a model rocket use to over come weight?

Thrust (due to solid or liquid fuel burning)


How many tons of rocket fuel does the shuttle use during liftoff?

The Space Shuttle used approximately 1.6 million pounds (800 tons) of solid rocket fuel during liftoff. This solid rocket fuel was primarily used in the twin solid rocket boosters that provided the initial thrust to launch the shuttle into space.


What force proples a rocket?

A rocket is propelled by the force generated through the controlled burning of rocket fuel. As the fuel burns, it is expelled out of the rocket's engine at high speed, creating thrust in the opposite direction that propels the rocket forward due to Newton's third law of motion.


How a solid fuel rocket start and stops?

A solid fuel rocket starts when igniters are activated, igniting the solid propellant within the rocket motor. This combustion produces high-pressure gases that are expelled through a nozzle, generating thrust and propelling the rocket upward. The rocket stops when the fuel is completely consumed, as there is no mechanism to shut off the combustion in solid propellant systems. Once the fuel is exhausted, the rocket coasts until it reaches the desired altitude or trajectory.