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Modeling of Heat Generation in Cryogenic Turbopump Bearing

Modeling of Heat Generation in Cryogenic Turbopump Bearing
Digital博士論文障害者向け資料あり
Kakudo, Hiromitsu2023-07-24
Available onlineNational Diet LibraryOther Libraries in Japan
  • Subject Heading液体ロケットエンジン 極低温ターボポンプ 転がり玉軸受 Liquid rocket engine cryogenic turbopump ba...

Mars flyer rocket propulsion risk assessment ARC testing [microform] ([NASA contractor report] ; NASA/CR-2001-210709)

Mars flyer rocket propulsion risk assessment ARC testing [microform] ([NASA contractor report] ; NASA/CR-2001-210709)
Microform図書
2001<YCA-NAS 1.26:210709>
National Diet Library
  • Subject HeadingLiquid rocket propellants Performance tests...

Catalyzed ignition of bipropellants in microtubes [microform] / Steven J. Schneider, George A. Boyarko and Chih-Jen Sung (NASA/TM-2003-212206)

Catalyzed ignition of bipropellants in microtubes [microform] / Steven J. Schneider, George A. Boyarko and Chih-Jen Sung (NASA/TM-2003-212206)
Microform図書
2003<YCA-NAS 1.15:212206>
National Diet Library
  • Subject Heading...ustion physics Liquid rocket propellants Low thrust propul...

Mars Flyer rocket propulsion risk assessment [microform] : Kaiser Marquardt testing / Kaiser Marquardt ; prepared under contract NAS3-99198 ([NASA contractor report] ; NASA/CR-2001-210710)

Mars Flyer rocket propulsion risk assessment [microform] : Kaiser Marquardt testing / Kaiser Marquardt ; prepared under contract NAS3-99198 ([NASA contractor report] ; NASA/CR-2001-210710)
Microform図書
2001<YCA-NAS 1.26:210710>
National Diet Library
  • Subject HeadingLiquid rocket propellants Performance tests...

Booster main engine selection criteria for the liquid fly-back booster [microform] / Richard M. Ryan, William J. Rothschild, and David L. Christensen (NASA/TM ; 208106)

Booster main engine selection criteria for the liquid fly-back booster [microform] / Richard M. Ryan, William J. Rothschild, and David L. Christensen (NASA/TM ; 208106)
Microform図書
1998<YCA-NAS 1.15:208106>
National Diet Library
  • Subject Heading...Rocket engines Liquid rocket propellants Booster rocket en...

Development of tripropellant CFD design code [microform] : contract no.--NAS8-40583 : final report / prepared by Richard C. Farmer, Gary C. Cheng, Peter G. Anderson

Development of tripropellant CFD design code [microform] : contract no.--NAS8-40583 : final report / prepared by Richard C. Farmer, Gary C. Cheng, Peter G. Anderson
Microform図書
1998<YCA-NAS 1.26:207893>
National Diet Library
  • Subject HeadingLiquid rocket propellants Computational flu...

アキシャルギャップモータによる液体ロケットエンジン電動ポンプへの可能性

アキシャルギャップモータによる液体ロケットエンジン電動ポンプへの可能性
Digital文書・図像類
島垣, 満, 木村, 俊哉, 髙田, 仁志, SHIMAGAKI, Mitsuru, KIMURA, Toshiya, TAKADA, Satoshi宇宙航空研究開発機構(JAXA)2023-01-20宇宙航空研究開発機構研究開発資料 = JAXA Research and Development MemorandumJAXA-RM-22-004p.1-10
Other Libraries in Japan
  • Subject HeadingAxial flux motor Single-shaft electric pump Liquid Rocket Engine
  • Alternative TitlePossibilities for a liquid rocket engine electric pump using an...
  • Alternative TitlePossibilities for a liquid rocket engine electric pump using an...

HAN-based monopropellant assessment for spacecraft [microform] / Robert S. Jankovsky (NASA technical memorandum ; 107287)

HAN-based monopropellant assessment for spacecraft [microform] / Robert S. Jankovsky (NASA technical memorandum ; 107287)
Microform図書
1996<YCA-NAS 1.15:107287>
National Diet Library
  • Subject HeadingMonopropellants Safety Liquid rocket propellants Launching Hydroxy...

"2001: a space Odyssey" revisited--the feasibility of 24 hour commuter flights to the moon using NTR propulsion with LUNOX afterburners [microform] / Stanley K. Borowski and Leonard A. Dudzinski (NASA/TM ; 1998-208830)

"2001: a space Odyssey" revisited--the feasibility of 24 hour commuter flights to the moon using NTR propulsion with LUNOX afterburners [microform] / Stanley K. Borowski and Leonard A. Dudzinski (NASA/TM ; 1998-208830)
Microform図書
1998<YCA-NAS 1.15:208830>
National Diet Library
  • Subject Heading...ropulsion Moon Liquid rocket propellants Space transportat...

Metallized gelled propellants [microform] : oxygen/RP-1/aluminum rocket heat transfer and combustion measurements / Bryan Palaszewski and James S. Zakany (NASA technical memorandum ; 107309)

Metallized gelled propellants [microform] : oxygen/RP-1/aluminum rocket heat transfer and combustion measurements / Bryan Palaszewski and James S. Zakany (NASA technical memorandum ; 107309)
Microform図書
1996<YCA-NAS 1.15:107309>
National Diet Library
  • Subject Heading...x quantization Liquid rocket propellants Metal propellants...

DRTS-1Nスラスタ軌道上推力低下事象の原因究明作業

DRTS-1Nスラスタ軌道上推力低下事象の原因究明作業
Digital文書・図像類
後藤, 大亮, 香河, 英史, 増田, 井出夫, 梶原, 堅一, 金森, 康郎, Goto, Daisuke, Kagawa, Hideshi, Masuda, Ideo, Kajiwara, Kenichi, Kanamori, Yasuro宇宙航空研究開発機構2006-11-01宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration AgencyJAXA-SP-06-006p.307-310
Other Libraries in Japan
  • Subject Heading...st measurement liquid rocket propellant hydrazine catalyst...

衛星用逆止弁不具合原因確認試験:シール変形確認試験

衛星用逆止弁不具合原因確認試験:シール変形確認試験
Digital文書・図像類
増田, 井出夫, 長田, 泰一, 梶原, 堅一, Masuda, Ideo, Nagata, Taiichi, Kajiwara, Kenichi宇宙航空研究開発機構2006-11-01宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration AgencyJAXA-SP-06-006p.303-306
Other Libraries in Japan
  • Subject Heading...ilure analysis liquid rocket propellant

酸素-メタン・燃料リッチプリバーナの燃焼特性

酸素-メタン・燃料リッチプリバーナの燃焼特性
Digital文書・図像類
小野, 文衛, 田村, 洋, 坂本, 博, 佐々木, 正樹, ONO, Fumiei, TAMURA, Hiroshi, SAKAMOTO, Hiroshi, SASAKI, Masaki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-11241124p.27-
Other Libraries in Japan
  • Subject Headingliquid rocket; LOX/methane; preburners; ...

C/C複合材を適用した高耐久性RCSスラスタの研究:SiC/C-FGM燃焼室耐久性評価試験

C/C複合材を適用した高耐久性RCSスラスタの研究:SiC/C-FGM燃焼室耐久性評価試験
Digital文書・図像類
佐藤, 政裕, 只野, 真, 日下, 和夫, 新野, 正之, 毛呂, 明夫, Sato, Masahiro, Tadano, Makoto, Kusaka, Kazuo, Niino, Masayuki, Moro, Akio航空宇宙技術研究所2001-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1427
Other Libraries in Japan
  • Subject Heading...ogen tetroxide liquid rocket propellant combustion chamber...

LE-7液酸ターボポンプインデューサの回転非同期軸振動の抑制

LE-7液酸ターボポンプインデューサの回転非同期軸振動の抑制
Digital文書・図像類
渡邉, 光男, 長谷川, 敏, 渡辺, 義明, 橋本, 知之, 吉田, 誠, 山田, 仁, Watanabe, Mitsuo, Hasegawa, Satoshi, Watanabe, Yoshiaki, Hashimoto, Tomoyuki, Yoshida, Makoto, Yamada, Hitoshi航空宇宙技術研究所1998-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1359p.1-16
Other Libraries in Japan
  • Subject Heading...ion H 2 rocket liquid rocket engine
  • Note (General)...p of the LE-7 (Liquid rocket Engine-7) engine, super synch...

デュアル混合比液酸/水素燃焼器の燃焼・熱負荷特性　1

デュアル混合比液酸/水素燃焼器の燃焼・熱負荷特性　1
Digital文書・図像類
坂本, 博, 佐々木, 正樹, 高橋, 守, 佐藤, 和雄, 田村, 洋, Sakamoto, Hiroshi, Sasaki, Masaki, Takahashi, Mamoru, Sato, Kazuo, Tamura, Hiroshi航空宇宙技術研究所1995-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1278p.1-15
Other Libraries in Japan
  • Subject Heading... mixture ratio liquid rocket fuel liquid ox......ion efficiency liquid rocket engine injector combustion pr...

LE-7用材料溶接継手の引張特性　(その1)

LE-7用材料溶接継手の引張特性　(その1)
Digital文書・図像類
橋本, 知之, 渡辺, 義明, 坂本, 光正, Hashimoto, Tomoyuki, Watanabe, Yoshiaki, Sakamoto, Mitsumasa航空宇宙技術研究所1992-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1188p.1-13
Other Libraries in Japan
  • Subject Heading...ce development liquid rocket engine microstructure Inconel...

ロケット-ラム複合燃焼器の実験

ロケット-ラム複合燃焼器の実験
Digital文書・図像類
佐藤, 和雄, 坂本, 博, 佐々木, 正樹, 小野, 文衛, 八柳, 信之, Sato, Kazuo, Sakamoto, Hiroshi, Sasaki, Masaki, Ono, Fumiei, Yatsuyanagi, Nobuyuki航空宇宙技術研究所1994-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1249p.1-17
Other Libraries in Japan
  • Subject Heading...流 相互作用効果 排気ノズル liquid rocket ramjet engine rocket ram comb...

Performance evaluation of LE-7 high pressure pumps

Performance evaluation of LE-7 high pressure pumps
Digital文書・図像類
吉田, 誠, 上條, 謙二郎, 長尾, 隆治, Yoshida, Makoto, Kamijo, Kenjiro, Nagao, Takaharu航空宇宙技術研究所1993-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1212Tp.1-8
Other Libraries in Japan
  • Subject Heading...能試験 turbo pump liquid rocket engine liquid oxygen liquid h...

液体酸素/高密度炭化水素/金属系ロケットエンジンの理論性能

液体酸素/高密度炭化水素/金属系ロケットエンジンの理論性能
Digital文書・図像類
佐藤, 和雄, 毛呂, 明夫, 八柳, 信之, 坂本, 博, Sato, Kazuo, Moro, Akio, Yatsuyanagi, Nobuyuki, Sakamoto, Hiroshi航空宇宙技術研究所1993-08航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory659p.1-10
Other Libraries in Japan
  • Subject Heading...ム マグネシウム 金属酸化物 liquid rocket engine liquid propellant fuel...
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