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ロケット用小型LH2ポンプの研究試作(その2)構造基本設計

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菊池, 正孝, 鈴木, 峰男, 志村, 隆, 渡辺, 光男, 上條, 謙二郎, 野坂, 正隆, 藁科, 彰吾, KIKUCHI, Masataka, SUZUKI, Mineo, SHIMURA, Takashi, WATANABE, Mitsuo, KAMIJO, Kenjiro, NOSAKA, Masataka, Shougo, Warashina航空宇宙技術研究所1991-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-11231123p.24-

Other Libraries in Japan

Subject HeadingRocket Pump; Liquid Hydrogen; Balance Piston; Self-Lubricated Bearing; S...
Note (General)...) for 350 s. A balance piston configuration ...... casing at the balance piston orifice. This positional disc...

LE-7液酸ターボポンプの軸推力釣合わせ

Digital文書・図像類

長谷川, 敏, 志村, 隆, Hasegawa, Satoshi, Shimura, Takashi航空宇宙技術研究所1993-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1201p.1-8

Other Libraries in Japan

Subject Heading...ancing chamber balance piston orifice balancing hole pressu...
Note (General)...eferred to as 'balance piston' was applied to the LE-7 LOX ...

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