GATE AE 2008 • Q30 MCQ • 1 Mark Propulsion

Propulsion

Rocket Propulsion

Subtopic: Tsiolkovsky Rocket Equation & Specific Impulse

Question Statement:

An aircraft is cruising at a true air speed (TAS) of 100 m/s under ISA conditions, at an altitude at which the density of free stream is 0.526 kg/m'. What will be the equivalent air speed (EAS)?

Options:

  • (A) 65.5 m/s
  • (B) 72.5 m/s
  • (C) 110.5 m/s
  • (D) 152.7 m/s

Official Answer Key:

B

Step-by-Step Solution & Explanation

### **Dedicated Step-by-Step Solution (GATE AE 2008 Q.30)** **1. Problem Statement & Parameters**: - **Module**: Propulsion (1 Mark, MCQ) - **Topic**: Rocket Propulsion (Tsiolkovsky Rocket Equation & Specific Impulse) - **Organizing Institute**: IISc Bengaluru - **Problem Statement**: > An aircraft is cruising at a true air speed (TAS) of 100 m/s under ISA conditions, at an altitude at which the density of free stream is 0.526 kg/m'. What will be the equivalent air speed (EAS)? **2. Mathematical Derivation & Physical Analysis**: 1. **Governing Physical Principles**: Governed by **Rocket Propulsion** (Tsiolkovsky Rocket Equation & Specific Impulse) under *Propulsion*. 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 **B**. **3. Comprehensive Options Analysis**: - **(A)** *"65.5 m/s"*: ❌ **INCORRECT**. - **(B)** *"72.5 m/s"*: ✅ **CORRECT**. - **(C)** *"110.5 m/s"*: ❌ **INCORRECT**. - **(D)** *"152.7 m/s"*: ❌ **INCORRECT**. **4. Official Answer Verification**: - **Official Master Answer**: **B** - **Evaluation Status**: Matches official GATE 2008 (IISc Bengaluru) master answer key with 100% precision.
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