Chapter 9: Problem 76
A \(6090 \mathrm{~kg}\) space probe moving nose-first toward Jupiter at \(105 \mathrm{~m} / \mathrm{s}\) relative to the Sun fires its rocket engine, ejecting \(80.0 \mathrm{~kg}\) of exhaust at a speed of \(253 \mathrm{~m} / \mathrm{s}\) relative to the space probe. What is the final velocity of the probe?
Short Answer
Step by step solution
Understand Conservation of Momentum
Define Initial Momentum
Calculate Initial Momentum
Define Final Momentum
Relative Velocities
Set Up Conservation Equation
Simplify the Equation
Solve for Final Velocity
Calculate Final Velocity
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Key Concepts
These are the key concepts you need to understand to accurately answer the question.
Space Probe
Some key features of space probes include:
- They lack life-support systems since they are not designed to carry humans.
- They are powered by solar panels or onboard generators.
- They communicate with Earth using radio signals.
Exhaust Velocity
In the context of our exercise:
- The space probe ejects exhaust gases at a velocity of 253 m/s relative to itself, which helps it to change its speed and direction.
- Exhaust velocity is pivotal in calculating the change in velocity of the space probe using the principle of conservation of momentum.
Rocket Propulsion
The key components involved in rocket propulsion include:
- Thrust: The force generated by the expulsion of gas to propel the rocket forward.
- Propellant: The material expelled from the rocket, which can be either liquid or solid.
- Exhaust Velocity: The speed at which the propellant is ejected, influencing the rocket's thrust and ultimately its velocity.