Newton's second law -- rockets

In summary, the conversation discusses the concept of force and acceleration in relation to Newton's second law and the rocket equation. It is explained that in the case of an isolated system, the net force between the mass inside and any mass outside the system is zero, resulting in zero acceleration. However, the rocket and the propellant within the system still experience opposite accelerations. The conversation also highlights the misconception of using the change in velocity of the rocket and the velocity of the propellant in the equation for momentum conservation. In short, the conversation emphasizes the importance of considering the entire system and using the principle of momentum conservation in understanding the dynamics of the rocket.
  • #1
Woopa
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4
I am having difficulty understanding the information below. In the second line it states that F=0 as there is no external force on the system. However it later calculates acceleration of the rocket.

How can Force=0 if there is acceleration? (This is the first time I have encountered the product rule so this may be part of my misunderstanding)

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  • #2
The keyword here is "system". By considering both the propellant (initial at rest inside the rocket) and the rocket itself to be part of the system and then say this system is isolated we are effectively saying that the net force between the mass inside and any mass outside the system is zero, leaving us to consider only forces between mass inside the system. This then means the momentum of the system is unchanged, or equivalently, if one part of the system, e.g. some of the propellant, accelerate one way then another part, e.g. the rocket plus its remaining propellant, has to accelerate in the opposite direction.
 
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  • #3
Woopa said:
Note that the "new form" of Newton's second law given here is not valid in general. There are several threads on here analysing this question.

In fact it's not really Newton's second law, but an equation that is only valid in this specific case.

PS the author has confusingly used the same letter ##v## for the velocity of the rocket and the velocity of the expellant. A simpler way to look at this is to use conservation of momentum:
$$m_r\Delta v_r + \Delta m_e v_e = 0$$Where we need the assumption that ##\Delta m_e## is small compared to ##m_r##. Otherwise, we would need to be more explicit that the mass of the rocket is changing from ##m_r + m_e## to ##m_r## after the expellent is fired out.
 
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  • #4
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  • #5
PS if we are being harsh, then the author has made two mistakes which cancel out and contrive to get the right equation:

1) Wrongly stating Newton's second law as ##F = m\frac{\Delta v}{\Delta t} + v\frac{\Delta m}{\Delta t}##.

2) Mistakingly using the change in velocity of the rocket as ##\Delta v## and the velocity of the expellant as ##v## in this equation.
 
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  • #6
Woopa said:
How can Force=0 if there is acceleration?
There is no acceleration. The rocket accelerates in one direction and the propellant accelerates in the opposite direction. The acceleration of the system (the system consisting of the rocket and the propellant) is zero.
 
  • #7

FAQ: Newton's second law -- rockets

What is Newton's second law of motion?

Newton's second law of motion states that the acceleration of an object is directly proportional to the net force acting upon it and inversely proportional to its mass. The law is commonly expressed with the equation F = ma, where F is the net force, m is the mass, and a is the acceleration.

How does Newton's second law apply to rockets?

Newton's second law applies to rockets by explaining how the force generated by the expulsion of exhaust gases results in the acceleration of the rocket. The force (thrust) produced by the rocket's engines is used to overcome the rocket's mass and any opposing forces, such as gravity and air resistance, resulting in acceleration.

What is thrust in the context of rocket propulsion?

Thrust is the force exerted by a rocket engine to propel the rocket forward. It is generated by expelling mass (exhaust gases) at high velocity in the opposite direction, according to Newton's third law of motion, which states that for every action, there is an equal and opposite reaction. Thrust is the action force that propels the rocket upward.

Why is mass important in Newton's second law for rockets?

Mass is important in Newton's second law for rockets because it directly affects the acceleration of the rocket. According to the equation F = ma, for a given force (thrust), a larger mass will result in a smaller acceleration, while a smaller mass will result in a larger acceleration. Therefore, reducing the rocket's mass or increasing the thrust can improve the rocket's acceleration.

How do rockets overcome Earth's gravity using Newton's second law?

Rockets overcome Earth's gravity by generating sufficient thrust to produce a net force greater than the gravitational force pulling them down. According to Newton's second law, this net force results in the rocket's acceleration. By continuously expelling exhaust gases and generating thrust, the rocket can accelerate upwards and eventually reach the necessary velocity to escape Earth's gravitational pull.

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