Designing and Modeling of Saturn V base on Juno New Origins

Abstract

Saturn V, utilized by NASA during the 1960s Apollo program, stands as a pivotal heavy-lift rocket in space exploration history. Its design and fabrication mark a significant chapter in spaceflight history. Through an amalgamation of Saturn V's authentic design parameters and Juno New Origins' sophisticated modeling tools, we proficiently resurrected this emblematic rocket system. This investigation delves into design methodology, model validation, and the advantages of Juno New Origins for Saturn V spacecraft modeling, offering a fresh vantage point for spacecraft design and simulation research. The modeling process spans four sections: S-IC, S-II, S-IVB, and supplementary modifications, exclusively utilizing Juno New Origins. Empirical evidence from user studies underscores the model's commendable quality and efficiency, bolstering its credibility within aerospace engineering. Evaluation outcomes reveal overwhelmingly positive sentiments regarding the model's performance, highlighting its efficacy in simulating diverse rocket interactions and its practical indispensability within aerospace engineering.