@article{oai:jaxa.repo.nii.ac.jp:00021724,
 author = {小川, 博之 and 野中, 聡 and 成尾, 芳博 and 伊藤, 隆 and 稲谷, 芳文 and Ogawa, Hiroyuki and Nonaka, Satoshi and Naruo, Yoshihiro and Ito, Takashi and Inatani, Yoshifumi},
 issue = {3},
 journal = {International Journal of Microgravity Science and Application (IJMSA)},
 month = {Jul},
 note = {The Reusable Sounding Rocket is a fully re-usable sub-orbital sounding rocket that takes-off and lands vertically from/on the same launch site. The Reusable Sounding Rocket recovers its payload: one can make repeated use of instruments, recover samples, have a big data storage onboard, and so on. The Reusable Sounding Rocket can be launched daily. The target cost for operation is 1/10 of the existing sounding rocket, S-310. The duration of μg environment is about 3 minutes. The payload bay is in the nose-cone and its volume is 0.8m in diameter and 1m in height. The maximum mass of the payload is 100kg., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: DS1640178000},
 pages = {330303-1--330303-5},
 title = {Reusable Sounding Rocket},
 volume = {33},
 year = {2016}
}