Insights How to Apply Newton’s Second Law to Variable Mass Systems

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SUMMARY

The discussion focuses on the application of Newton's Second Law, specifically the equation $$\frac{d\mathbf{P}}{dt}=\mathbf{F}_{\text{ext}}$$, in variable mass systems such as rockets. A critical example involves a rocket hovering above the Earth's surface while expelling combustion gases at a constant rate, denoted as ##\beta=dm/dt##. The confusion arises when novices misapply this equation, leading to incorrect conclusions about the conditions necessary for the rocket to maintain its position. The correct approach requires understanding the relationship between mass loss and the forces acting on the system.

PREREQUISITES
  • Understanding of Newton's Second Law and its general form
  • Familiarity with variable mass systems, particularly in the context of rocket dynamics
  • Knowledge of momentum and its relation to force
  • Basic principles of fluid dynamics as they apply to exhaust gases
NEXT STEPS
  • Study the derivation of the rocket equation in variable mass systems
  • Learn about the implications of mass flow rates on thrust generation
  • Explore advanced topics in fluid dynamics related to rocket propulsion
  • Investigate real-world applications of Newton's laws in aerospace engineering
USEFUL FOR

Students of physics, aerospace engineers, and anyone interested in the dynamics of variable mass systems, particularly in the context of rocket science.

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Introduction
The applicability of Newton’s second law in the oft-quoted “general form”  $$\begin{align}\frac{d\mathbf{P}}{dt}=\mathbf{F}_{\text{ext}}\end{align}$$ was an issue in a recent thread (see post #4) in cases of systems with variable mass.  The following example illustrates the kind of confusion that could arise from the (mis)application of Equation (1):
A rocket is hovering in place above ground near the Earth’s surface. Assume that the combustion gases are expelled at constant rate ##\beta=dm/dt## with velocity ##w## relative to the rocket.  What condition must hold for the rocket to hover in place?
A novice might start with Equation (1) and go down the garden path only to reach a quick impasse as shown below.
Attempted solution
We start with the general form of Newton’s second law, Equation (1) $$\frac{dP}{dt}=M\frac{dV}{dt}+V\frac{dM}{dt}=-Mg$$ If...

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