Rocket Propulsion Gas Injection

In summary, the conversation discusses the calculation of how much gas a rocket must eject in the first second to have an initial acceleration of 25.0 m/s^2 in deep space with negligible gravity. The hint given is to use conservation of momentum and the question asks for the answer to this calculation.
  • #1
ada0289
2
0
Please help, book gives no examples relatively close to this.

A rocket is fired in deep space, where gravity is negligible.


If the rocket has an initial mass of 6000 kg and ejects gas at a relative velocity of magnitude 2000 m/s , how much gas must it eject in the first second to have an initial acceleration of 25.0 m/s^2?
 
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  • #2
Welcome to PF!

Hi ada0289! Welcome to PF! :smile:
ada0289 said:
If the rocket has an initial mass of 6000 kg and ejects gas at a relative velocity of magnitude 2000 m/s , how much gas must it eject in the first second to have an initial acceleration of 25.0 m/s^2?

Hint: use conservation of momentum :wink:

What do you get? :smile:
 
  • #3


To determine the amount of gas that must be ejected in the first second for the rocket to have an initial acceleration of 25.0 m/s^2, we can use the equation F = ma, where F is the force, m is the mass, and a is the acceleration.

Since we know the initial mass of the rocket (6000 kg) and the desired initial acceleration (25.0 m/s^2), we can rearrange the equation to solve for the force: F = ma = (6000 kg)(25.0 m/s^2) = 150,000 N.

Now, to calculate the force generated by the gas ejection, we can use the equation F = Δp/Δt, where Δp is the change in momentum and Δt is the time interval.

Since the rocket ejects gas at a relative velocity of 2000 m/s, the change in momentum can be calculated as Δp = (6000 kg)(2000 m/s) = 12,000,000 kg·m/s. Assuming the gas is ejected in the first second, the time interval Δt would be 1 second.

Plugging these values into the equation, we get: F = Δp/Δt = (12,000,000 kg·m/s) / (1 s) = 12,000,000 N.

Therefore, in order for the rocket to have an initial acceleration of 25.0 m/s^2, it would need to eject gas with a total force of 12,000,000 N in the first second. This amount of gas can then be converted into a mass using the equation F = ma, where F is the force calculated (12,000,000 N), m is the mass of the gas, and a is the acceleration of the gas (2000 m/s^2).

Thus, the amount of gas ejected in the first second would be approximately 6 kg. This calculation shows that even a small amount of gas ejected at a high velocity can generate a significant amount of force and contribute to the rocket's acceleration.
 

Related to Rocket Propulsion Gas Injection

1. What is rocket propulsion gas injection?

Rocket propulsion gas injection is a method used in rocket engines to inject gas, such as hydrogen or oxygen, into the combustion chamber to create thrust. This helps to increase the efficiency and power of the engine.

2. How does rocket propulsion gas injection work?

Rocket propulsion gas injection works by injecting gas at a specific rate into the combustion chamber, where it mixes with the fuel and ignites. This creates a controlled explosion, which produces the thrust needed to propel the rocket forward.

3. What types of gas are commonly used in rocket propulsion gas injection?

The most commonly used gases in rocket propulsion gas injection are hydrogen and oxygen. These gases have high energy densities and can be easily stored in liquid form, making them ideal for use in rocket engines.

4. What are the benefits of using rocket propulsion gas injection?

There are several benefits to using rocket propulsion gas injection, including increased efficiency and power of the engine, improved control and stability, and the ability to use a wider range of fuels. It also allows for more precise adjustments to the thrust, making it easier to control the rocket's trajectory.

5. What are some challenges associated with rocket propulsion gas injection?

One of the main challenges of rocket propulsion gas injection is the complexity of the system. It requires precise control and synchronization of multiple components, which can be difficult to achieve. There are also challenges related to the storage and handling of the gases, as they are highly explosive and require strict safety measures.

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