RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing

Fuente: arXiv
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Autori principali: Pak, Peter, Barkley, Jesse, Loghmani, Rumi, Baich, Derek, Pamal, Ananya, Farimani, Amir Barati
Natura: Preprint
Pubblicazione: 2026
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author Pak, Peter
Barkley, Jesse
Loghmani, Rumi
Baich, Derek
Pamal, Ananya
Farimani, Amir Barati
author_facet Pak, Peter
Barkley, Jesse
Loghmani, Rumi
Baich, Derek
Pamal, Ananya
Farimani, Amir Barati
contents This work presents RocketSmith, an agentic system capable of the design, manufacturing, and optimization processes in high powered rocket development. The system enables the intelligent automation of software tools as to not only validate factors such as flight stability but also generate the parametric design components for the rocket assembly. A collection of subagents and skills enable optimization workflows of flight parameters via iteration in both zero-shot and human-in-the-loop workflows. With this system, four distinct high power rockets with various motor and assembly configurations were developed utilizing the unique design capabilities of additive manufacturing. These assembly components were fabricated using various FDM printers, manually evaluated for flight readiness, and flight tested at a launch event. From these tests, all rockets achieved a stable launched and two of the four rockets were successfully recovered in reflyable condition. Within the collected flight data, an 84% accuracy was achieved when comparing measured apogee to that calculated in flight simulations.
format Preprint
id arxiv_https___arxiv_org_abs_2606_00097
institution arXiv
publishDate 2026
record_format arxiv
spellingShingle RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing
Pak, Peter
Barkley, Jesse
Loghmani, Rumi
Baich, Derek
Pamal, Ananya
Farimani, Amir Barati
Robotics
This work presents RocketSmith, an agentic system capable of the design, manufacturing, and optimization processes in high powered rocket development. The system enables the intelligent automation of software tools as to not only validate factors such as flight stability but also generate the parametric design components for the rocket assembly. A collection of subagents and skills enable optimization workflows of flight parameters via iteration in both zero-shot and human-in-the-loop workflows. With this system, four distinct high power rockets with various motor and assembly configurations were developed utilizing the unique design capabilities of additive manufacturing. These assembly components were fabricated using various FDM printers, manually evaluated for flight readiness, and flight tested at a launch event. From these tests, all rockets achieved a stable launched and two of the four rockets were successfully recovered in reflyable condition. Within the collected flight data, an 84% accuracy was achieved when comparing measured apogee to that calculated in flight simulations.
title RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing
topic Robotics
url https://arxiv.org/abs/2606.00097