Austin Heisey (Project Manager) - 2nd year Software Engineer
Brahm Soltes - 2nd year Mechanical Engineer
Jacob Cole - 1st year Mechanical Engineer
Joy Sangsrichan - 2nd year Computer Science
Pieter Van Zeijts - 1st year Mechanical Engineer
Seth Davidson - 1st year Electrical Engineer
A minimum diameter 54mm L class motor rocket with an expected altitude of 32,030 ft. Our goals are to beat the Tripoli record for an L class motor and to take a 360-degree video from launch to apogee.
Loaded Mass: 143 oz.
Inner Diameter: 2.142 in.
Outer Diameter: 2.31 in.
Airframe Length: 55.14 in.
Airframe Diameter: 54mm.
Stability: 2.33 cal.
Max Speed: 2,744 ft/s
Target Apogee: 33,324 ft/s
Preliminary Design Review
The team received good feedback during the preliminary design review (PDR).
Critical Design Review
The team's design was approved, and the team will start construction.