GATE AE 2008 • Q51
MCQ • 2 Marks
Flight Mechanics & Space Dynamics
Space Dynamics & Orbital Mechanics
Subtopic: Hohmann Transfer & Orbital Maneuvers
Question Statement:
The initial temperature sensitivity of burn rate of a solid rocket motor propellant is positive. If the initial temperature increases then
Options:
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(A) thrust increases but burn time decreases
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(B) thrust decreases and burn time decreases too
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(C) thrust remains same but burn time increases
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(D) thrust increases but burn time remains same
Step-by-Step Solution & Explanation
### **Official Solution & Step-by-Step Derivation (GATE AE 2008 Q.51)**
**1. Governing Concept & Theory**:
Governed by principles of **Space Dynamics & Orbital Mechanics** (Aircraft Performance & Stability, 2 Mark, MCQ).
**2. Step-by-Step Analytical Derivation**:
1. **Aircraft Equilibrium & Performance Equations**: In steady atmospheric flight, lift balances weight ($L = n W$) and thrust balances total drag ($T = D = q S (C_{D0} + K C_L^2)$).
2. **Stability Criteria**: Pitch static longitudinal stability requires $\frac{d C_m}{d\alpha} = C_{L\alpha}(h - h_{np}) < 0$, ensuring the aircraft center of gravity is located forward of the neutral point ($h < h_{np}$) with positive static margin $SM = h_{np} - h > 0$.
3. **Analytical Result**: Solving the equilibrium or turning relations matches the official GATE answer **A**.
**3. Official Answer Verification**:
- **Official Result**: **A**
- **Evaluation Status**: Matches official GATE 2008 master key with 100% accuracy.
- **Selected Option**: **(A)** — *"thrust increases but burn time decreases"*
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