The document summarizes the design of a rocket for a competition to reach 10,000 feet carrying a 10 pound payload. Key aspects of the design include: 1) A carbon fiber fuselage and internal damping structure for the rocket structure. 2) Use of a commercially available motor (Aerotech M1350-P) to ensure sufficient impulse for the target altitude, as non-COTS fuel mixtures did not provide consistent performance. 3) Tangent ogive nose cone and trapezoidal fins to minimize drag while maintaining stability, allowing the target apogee to be reached. 4) Dual deployment recovery system using drogue and main parachutes to control descent and prevent drifting more