RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing
arXiv:2606.00097v1 Announce Type: new Abstract: 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.
[2606.00097] RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing
[Submitted on 25 May 2026]
Title:RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing
View a PDF of the paper titled RocketSmith: An Agentic System for High-Powered Rocket Design and Manufacturing, by Peter Pak and 5 other authors
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Abstract: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.
Subjects:
Robotics (cs.RO)
Cite as: arXiv:2606.00097 [cs.RO]
(or arXiv:2606.00097v1 [cs.RO] for this version)
https://doi.org/10.48550/arXiv.2606.00097
arXiv-issued DOI via DataCite
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From: Peter Pak [view email] [v1] Mon, 25 May 2026 14:37:39 UTC (25,980 KB)
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