GATE AE 2010 • Q25
MCQ • 1 Mark
Flight Mechanics & Space Dynamics
Space Dynamics & Orbital Mechanics
Subtopic: Kepler's Laws & Two-Body Problem
Question Statement:
Ignoring compressibility effects, the cruising speed of the aircraft is approximately
Options:
-
(A) 50 m/s
-
(B) 100 m/s
-
(C) 150 m/s
-
(D) 200 m/s
Step-by-Step Solution & Explanation
### **Dedicated Step-by-Step Solution (GATE AE 2010 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 Guwahati
- **Problem Statement**:
> Ignoring compressibility effects, the cruising speed of the aircraft is approximately
**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)** *"50 m/s"*: ❌ **INCORRECT**.
- **(B)** *"100 m/s"*: ❌ **INCORRECT**.
- **(C)** *"150 m/s"*: ✅ **CORRECT**.
- **(D)** *"200 m/s"*: ❌ **INCORRECT**.
**4. Official Answer Verification**:
- **Official Master Answer**: **C**
- **Evaluation Status**: Matches official GATE 2010 (IIT Guwahati) master answer key with 100% precision.
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