Problem 1.45 — Acceleration of the Moon — centripetal from orbital data

Problem Statement

Solve the Newton’s Laws / mechanics problem: The Moon orbits Earth at $R = 3.84\times10^5\,\text{km}$ with period $T = 27.3\,\text{days}$. Find the Moon’s centripetal acceleration and compare with $g$ at Earth’s surface. Angular velocity: $$\omega = \frac{2\pi}{T} = \frac{2\pi}{27.3\times86400} = 2.66\times10^{-6}\,\text{rad/s}$$ Centripetal a

Given Information

  • $T = 27.3\,\text{days}$

Physical Concepts & Formulas

Circular motion requires a centripetal force directed toward the centre, providing the centripetal acceleration $a_c = v^2/r = \omega^2 r$. This force is not a new type of force — it is always the resultant of real forces (tension, normal force, friction, gravity) directed inward. At the minimum speed for maintaining contact, the normal force drops to zero.

  • $a_c = v^2/R = \omega^2 R$ — centripetal acceleration
  • $F_c = mv^2/R$ — net centripetal force needed
  • Banked curve: $\tan\theta = v^2/(Rg)$ — ideal banking angle
  • Loop minimum speed: $v_{\min} = \sqrt{gR}$ at top (N=0)

Step-by-Step Solution

Step 1 — Verify the result: Check units, limiting cases, and order of magnitude to confirm the answer is physically reasonable.

Step 2 — Verify the result: Check units, limiting cases, and order of magnitude to confirm the answer is physically reasonable.

Step 3 — Verify the result: Check units, limiting cases, and order of magnitude to confirm the answer is physically reasonable.

Worked Calculation

$$\omega = \frac{2\pi}{T} = \frac{2\pi}{27.3\times86400} = 2.66\times10^{-6}\,\text{rad/s}$$

$$\sum F_x = ma_x\quad,\quad \sum F_y = ma_y = 0\quad\text{(if no vertical acceleration)}$$

$$a = \frac{(m_2-m_1)g}{m_1+m_2} = \frac{(5-3)\times9.8}{8} = \frac{19.6}{8} = 2.45\,\text{m/s}^2$$

Answer

$$\boxed{a = \dfrac{(m_2-m_1)g}{m_1+m_2}}$$

Physical Interpretation

The centripetal force is not a ‘new’ force but the net inward resultant of real forces. If that resultant falls below $mv^2/r$, the object cannot maintain circular motion and will fly outward — this is the critical condition for minimum speed problems.


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