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This document outlines the critical design review for the Student Launch Project conducted on February 28, 2014. It details the final specifications for team structure, launch vehicle dimensions, motor choices at various altitudes, and key performance metrics such as static stability margin, thrust-to-weight ratio, and mass statements. Additionally, it includes plans and procedures for recovery system tests, parachute, airframe materials, and wind tunnel tests, as well as verification of flight tests, ensuring all components meet operational safety and performance standards.
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Student Launch Project Critical Design Review February 28, 2014
Predicted Drift from Launch Pad 18,00 ft. Flight 9,000 ft. Flight
Test Plans and Procedures • Recovery System Tests • Ensure safe operation of recovery system • Parachute tests, static ejection tests, bulkhead tests • Airframe Materials Tests • Verify that airframe components can withstand expected loads • Tests to failure, including tensile and compressive tests • Wind Tunnel Tests • Tests to find drag coefficient for increased accuracy of simulations • Nylon Bolts • Tests to determine the correct amount of black powder to be placed in Nylon Exploding Bolts • Electrical Components • Tests to ensure minimum amount of error.