@inproceedings{oai:jaxa.repo.nii.ac.jp:00038586,
 author = {増田, 井出夫 and 藤井, 剛 and 毛利, 和生 and 草間, 光治 and Masuda, Ideo and Fujii, Go and Mouri, Kazuo and Kusama, Mitsuharu},
 book = {第57回宇宙科学技術連合講演会講演集, Proceedings of 57th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県, We choose a new type of Plug cluster nozzle for satellites, from the perspective of improved performance within the restricted installation area of rockets. The new nozzles are considered much more efficient for the larger nozzle expansion area ratio than existing ones. Given the concerns over degraded performance due to a slower flow of exhaust gas caused by shock waves in the overlapped area between the modules that constitute a cluster nozzle, we evaluated the effect of each module’s overlap ratio on nozzle performance based on an examination using nitrogen gas. Our experimental and analytical results by cold gas revealed that the plug cluster nozzle having a low overlap ratio offers better performance than the bell nozzle having the same effective expansion ratio. In order to understand the combustion gas characteristics of the plug cluster nozzle, we plan to perform firing tests. We describe the firing test nozzle and test equipment in this paper., 資料番号: AC1400002000, レポート番号: JSASS-2013-4271},
 publisher = {日本航空宇宙学会, The Japan Society for Aeronautical and Space Sciences},
 title = {人工衛星用プラグクラスタノズルの燃焼ガス試験計画},
 year = {2013}
}