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.
Poster the team is presenting at Imagine RIT