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Autor:
Harunori Nagata, Hiroyuki Yasukochi, Tsuyoshi Totani, Ryuichiro Kanai, Yuji Saito, Masashi Wakita, Hayato Teraki
Publikováno v:
51st AIAA/SAE/ASEE Joint Propulsion Conference.
The authors have previously proposed the concept of end-burning-type hybrid rockets, which would use cylindrical fuel grains consisting of an array of many small ports running in the axial direction, through which oxidizer gas would flow. Because of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1e73a8ad7e94d6fcfd044d10e7940c61
https://doi.org/10.2514/6.2015-4199
https://doi.org/10.2514/6.2015-4199
