It’s official! Team A.R.C. has completed our Final Design Review (FDR) for the IPPD program, and we couldn’t be prouder of what we’ve accomplished over these past two semesters.

When we set out to tackle the growing problem of low Earth orbit space debris, we knew we needed an innovative approach. Through our custom S.M.A.R.T. (Simulation and Machine-learning Assisted Redesign and Testing) methodology, we successfully replaced traditional trial-and-error with an automated, data-driven design loop. By utilizing Kriging algorithms and rigorous hypersonic simulations, our team converged on an optimal Magnesium chassis with deployable flaps engineered to induce violent shock-shock interference intentionally. Proving that our architecture can capture 64.5 megawatts of heat and spike structural temperatures to 1,555 K during a Mach 20 descent is a massive win for the future of sustainable Design for Demise aerospace engineering.
Of course, this milestone would not have been possible without the support of Honeywell Aerospace Technologies. We also want to extend a massive, heartfelt thank you to our liaison engineers: Joseph McMahan and Caleb Sjoquist. Thank you. We also owe a huge thanks to our Faculty Coach, Dr. Rick Lind, for guiding us every step of the way.
As we hand off our baseline geometries and physical prototypes, we are incredibly excited to see where Honeywell takes this technology next. Here’s to a cleaner orbit and a successful end to an unforgettable project!













