You send a probe to orbit Mercury at 192 km above the surface. What orbital velocity (in km/s) is needed to keep it in orbit? (The mass of Mercury is 3.30 x 1023 kg, and the radius of Mercury is 2.44 × 103 km.)
You send a probe to orbit Mercury at 192 km above the surface. What orbital velocity (in km/s) is needed to keep it in orbit? (The mass of Mercury is 3.30 x 1023 kg, and the radius of Mercury is 2.44 × 103 km.)
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![**Tutorial: Orbital Dynamics and Communication with Mercury**
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**Scenario:**
You send a probe to orbit Mercury at 192 km above the surface.
1. **Orbital Velocity Calculation:**
- What orbital velocity (in km/s) is required to keep the probe in orbit?
- **Given Data:**
- Mass of Mercury: \(3.30 \times 10^{23}\) kg
- Radius of Mercury: \(2.44 \times 10^3\) km
2. **Signal Time Comparison:**
- Calculate the ratio of the time it takes for a signal to travel from Earth to Mercury \((d = 57.9 \times 10^6\) km) to the time it takes to reach the Moon \((d = 384,400\) km).
3. **Wavelength Shift Calculation:**
- Given a signal at 15 cm, determine the wavelength shift (in cm) at this orbital velocity.
- **Assumption:** The probe is moving directly away from Earth.
---
**Part 1 of 4: Calculating Orbital Velocity**
- The orbital velocity (\(v_c\)) is equivalent to the circular velocity, defined by:
\[
v_c = \sqrt{\frac{GM}{r}}
\]
where \(G\) is the gravitational constant, \(M\) is the mass of Mercury, and \(r\) is the distance from the center of Mercury (radius of Mercury plus the altitude of the orbit).
- The equation specifies:
- \(v_c = \sqrt{\frac{GM_{\text{Mercury}}}{r}}\)
- This equation is used to calculate the velocity in km/s necessary for maintaining orbit at the specified height.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fda14446f-ef4d-47d5-9b14-b7a32b5fa1b1%2F2a57659f-8463-405a-80a4-1fceba283479%2Fh6uvsr_processed.jpeg&w=3840&q=75)
Transcribed Image Text:**Tutorial: Orbital Dynamics and Communication with Mercury**
---
**Scenario:**
You send a probe to orbit Mercury at 192 km above the surface.
1. **Orbital Velocity Calculation:**
- What orbital velocity (in km/s) is required to keep the probe in orbit?
- **Given Data:**
- Mass of Mercury: \(3.30 \times 10^{23}\) kg
- Radius of Mercury: \(2.44 \times 10^3\) km
2. **Signal Time Comparison:**
- Calculate the ratio of the time it takes for a signal to travel from Earth to Mercury \((d = 57.9 \times 10^6\) km) to the time it takes to reach the Moon \((d = 384,400\) km).
3. **Wavelength Shift Calculation:**
- Given a signal at 15 cm, determine the wavelength shift (in cm) at this orbital velocity.
- **Assumption:** The probe is moving directly away from Earth.
---
**Part 1 of 4: Calculating Orbital Velocity**
- The orbital velocity (\(v_c\)) is equivalent to the circular velocity, defined by:
\[
v_c = \sqrt{\frac{GM}{r}}
\]
where \(G\) is the gravitational constant, \(M\) is the mass of Mercury, and \(r\) is the distance from the center of Mercury (radius of Mercury plus the altitude of the orbit).
- The equation specifies:
- \(v_c = \sqrt{\frac{GM_{\text{Mercury}}}{r}}\)
- This equation is used to calculate the velocity in km/s necessary for maintaining orbit at the specified height.
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