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Imagine that you are in a spacecraft orb...

Imagine that you are in a spacecraft orbiting around the earth in a circle of radius `7000 km` (from the centre of the earth). If you decrease the magnitude of mechanical energy of the spacecraft `-` earth system by `10%` by firing the rockets, then what is the greatest height you can take your spacecraft above the surface of the earth? [`R_(e) = 6400 km`]

A

(a)`6400 km`

B

(b)`540km`

C

(c)`2140 km`

D

(d)`3000 km`

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem, we need to determine the greatest height a spacecraft can reach above the Earth's surface after decreasing its mechanical energy by 10%. ### Step-by-Step Solution: 1. **Identify the Given Values:** - Radius of Earth, \( R_e = 6400 \, \text{km} \) - Radius of orbit, \( r = 7000 \, \text{km} \) - Decrease in mechanical energy = 10% 2. **Calculate the Initial Mechanical Energy:** The mechanical energy \( E \) of a spacecraft in orbit is given by: \[ E = -\frac{G M m}{2r} \] where \( G \) is the gravitational constant, \( M \) is the mass of the Earth, and \( m \) is the mass of the spacecraft. 3. **Calculate the New Mechanical Energy:** If the mechanical energy is decreased by 10%, the new energy \( E' \) is: \[ E' = E - 0.1E = 0.9E \] Substituting the expression for \( E \): \[ E' = 0.9 \left(-\frac{G M m}{2r}\right) = -\frac{0.9 G M m}{2r} \] 4. **Set Up the Equation for the New Orbit:** The new mechanical energy in a different orbit (with radius \( r' \)) can be expressed as: \[ E' = -\frac{G M m}{2r'} \] Setting the two expressions for \( E' \) equal gives: \[ -\frac{0.9 G M m}{2r} = -\frac{G M m}{2r'} \] 5. **Simplify the Equation:** Canceling out common terms: \[ \frac{0.9}{r} = \frac{1}{r'} \] Rearranging gives: \[ r' = \frac{r}{0.9} = \frac{7000 \, \text{km}}{0.9} \approx 7777.78 \, \text{km} \] 6. **Calculate the Greatest Height Above the Earth's Surface:** The height \( h \) above the Earth's surface is given by: \[ h = r' - R_e \] Substituting the values: \[ h = 7777.78 \, \text{km} - 6400 \, \text{km} \approx 1377.78 \, \text{km} \] ### Final Answer: The greatest height the spacecraft can reach above the surface of the Earth is approximately **1377.78 km**.

To solve the problem, we need to determine the greatest height a spacecraft can reach above the Earth's surface after decreasing its mechanical energy by 10%. ### Step-by-Step Solution: 1. **Identify the Given Values:** - Radius of Earth, \( R_e = 6400 \, \text{km} \) - Radius of orbit, \( r = 7000 \, \text{km} \) - Decrease in mechanical energy = 10% ...
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