Yoshitaka Saito, Daisuke Akita, Issei Iijima, Chusaku Ikeda, Ayumu Ikuta, Hideyuki Fuke, Tatsuya Furuta, Hideyuki Mori, Keita Mizukoshi, Yoshitaka Mizumura, Makoto Tamura, Masahiro Yamatani, Daisuke Akita, Kyoichi Nakashino, Takuma Matsuo, Yutaka Igarashi, Hiroyuki Hashimoto, Kiyoho Matsushima
45th COSPAR Scientific Assembly 2024年7月16日
This study addresses the challenge of slit-like hole generation due to impact damage in super-pressure balloons covered by nets, with a specific focus on the NPB2-3 model. Despite its advanced and lightweight design optimized for high-altitude flights, the launching process revealed a significant vulnerability: rapid contact between the net and the balloon film upon the spooler's release, leading to numerous slit-like holes and characteristic film damage. To tackle this issue, a quasi-static launch method was developed and evaluated to minimize stress on the balloon film. This method is characterized by a technical innovation that involves setting an additional retention point, apart from the tail, to maintain the collar position during gas filling. Results from a series of experiments, including a simulated launch test using the NPB2-4 model, demonstrated a significant reduction in damage, ultimately achieving complete prevention of slit-like holes. This paper presents the methodology, experimental setup, and results, and discusses the application of this method to the upcoming NPB2-5 model launch in 2024, as well as its potential extension to other balloon launches.