Mission
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Our mission is to build a minimum diameter 54mm rocket that will break the current Tripoli altitude record (32,030 ft.) for an L class motor. |
Team Overview
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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 |
Project Adamson
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.
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Vehicle Summary
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
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Poster the team is presenting at Imagine RIT
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