A 2.0x10^4 kg rocket has a rocket motor that generates….

In summary, the mass of the rocket is 2.0x10^4 kg, which is enough to generate the required thrust needed for liftoff. The mass also affects the amount of fuel needed for the journey. The rocket can be considered heavy in comparison to smaller space exploration rockets, but is relatively light compared to larger commercial rockets. The rocket motor can be adjusted to generate more or less thrust by controlling the amount of fuel and oxidizer used.
  • #1
Cb8
4
1
Homework Statement
A 2.0x104 kg rocket has a rocket motor that
generates 2.7×105 N of thrust.
A) What is the rocket's initial upward acceleration in m/s^2.

B) At an altitude of 5000 m the rocket's acceleration has
increased to 6.0 m/s?. What mass of fuel has it
burned in kg.
Relevant Equations
2.0x10^4 kg Rocket
2.7x10^5 N of thrust
I tried A with the solution of 9.73 and 8.69 both wrong.
 
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  • #2
Cb8 said:
Homework Statement:: A 2.0x104 kg rocket has a rocket motor that
generates 2.7×105 N of thrust.
A) What is the rocket's initial upward acceleration in m/s^2.

B) At an altitude of 5000 m the rocket's acceleration has
increased to 6.0 m/s?. What mass of fuel has it
burned in kg.
Relevant Equations:: 2.0x10^4 kg Rocket
2.7x10^5 N of thrust

I tried A with the solution of 9.73 and 8.69 both wrong.
Please explain how you arrived at those solutions.
 

1. How does the weight of the rocket affect its performance?

The weight of the rocket is a crucial factor in determining its performance. A heavier rocket will require more fuel to lift off and reach its desired altitude, resulting in a shorter flight time and reduced overall efficiency. On the other hand, a lighter rocket will be able to achieve higher speeds and greater distances.

2. How does the rocket motor generate thrust?

The rocket motor generates thrust through the process of combustion. Fuel and oxidizer are mixed and ignited, producing hot gases that are expelled through the nozzle at high speeds. This action creates an equal and opposite force, propelling the rocket forward.

3. What is the significance of the 2.0x10^4 kg measurement?

This measurement refers to the mass of the rocket, which is a crucial factor in determining its overall performance. The mass of the rocket directly affects its acceleration, speed, and fuel consumption. It is important for engineers to carefully consider the mass of the rocket when designing and building it.

4. How does the rocket motor's power affect the rocket's trajectory?

The power of the rocket motor, or the amount of thrust it generates, plays a significant role in determining the rocket's trajectory. A more powerful motor will result in a greater amount of thrust, allowing the rocket to reach higher altitudes and travel further distances. However, a less powerful motor may be more suitable for a specific mission that requires more precise control over the rocket's trajectory.

5. Can the rocket motor's power be adjusted during flight?

In most cases, the power of the rocket motor cannot be adjusted during flight. However, some advanced rockets may have the capability to adjust the thrust of their motors through the use of thrust vectoring or throttle control. This allows for more precise control over the rocket's trajectory and can be useful in certain situations.

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