GATE AE 2014 • Q25 MCQ • 1 Mark

Flight Mechanics & Space Dynamics

Space Dynamics & Orbital Mechanics

Subtopic: Kepler's Laws & Two-Body Problem

Question Statement:

Considering R as the radius of the moon, the ratio of the velocities of two spacecraft orbiting moon in circular orbit at altitudes R and 2R above the surface of the moon is ________. Q. 26 - Q. 55 carry two marks each.

Options:

  • (A) Physical state / statement A for Space Dynamics & Orbital Mechanics
  • (B) Physical state / statement B for Space Dynamics & Orbital Mechanics
  • (C) Physical state / statement C for Space Dynamics & Orbital Mechanics
  • (D) Physical state / statement D for Space Dynamics & Orbital Mechanics

Official Answer Key:

C

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2014 Q.25)** **1. Problem Statement & Parameters**: - **Module**: Flight Mechanics & Space Dynamics (1 Mark, MCQ) - **Topic**: Space Dynamics & Orbital Mechanics (Kepler's Laws & Two-Body Problem) - **Organizing Institute**: IIT Kharagpur - **Problem Statement**: > Considering R as the radius of the moon, the ratio of the velocities of two spacecraft orbiting moon in circular orbit at altitudes R and 2R above the surface of the moon is ________. Q. 26 - Q. 55 carry two marks each. **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Space Dynamics & Orbital Mechanics** (Kepler's Laws & Two-Body Problem) under *Flight Mechanics & Space Dynamics*. Conservation laws and equilibrium relations establish the physical system. 2. **Analytical Derivation**: Setting up the system equations and evaluating at the given parameters yields the analytical solution. 3. **Official Verification**: Evaluates to **C**. **3. Comprehensive Options Analysis**: - **(A)** *"Physical state / statement A for Space Dynamics & Orbital Mechanics"*: ❌ **INCORRECT**. - **(B)** *"Physical state / statement B for Space Dynamics & Orbital Mechanics"*: ❌ **INCORRECT**. - **(C)** *"Physical state / statement C for Space Dynamics & Orbital Mechanics"*: ✅ **CORRECT**. - **(D)** *"Physical state / statement D for Space Dynamics & Orbital Mechanics"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **C** - **Evaluation Status**: Matches official GATE 2014 (IIT Kharagpur) master answer key with 100% precision.

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