-
1
المؤلفون: Atsumi, Masahiro, Ogawara, Akira, Warashina, Shogo, Iwama, Kazuyoshi
المصدر: 宇宙輸送シンポジウム 平成14年度 = Proceedings of Space Transportation Symposium FY2002. :99-102
مصطلحات موضوعية: H-2A打上げ機, 信頼性, H-2A rocket, reliability, LE-7Aエンジン, high thrust, expander engine, rocket engine, Japanese space program, research and development, LE-7A engine, タービンパンプ, turbine pump, 高推力, 日本の宇宙開発プログラム, ロケットエンジン, エキスパンダエンジン, 研究開発
URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::8962aaf58d0031a6eceb443980d3a5a5
http://id.nii.ac.jp/1696/00017355/ -
2
المؤلفون: Louaas, Eric, Talbot, Chrsistoph, Gonzalez Gotor, Pilar, Ruiz Merino, Alejandro, Longo, Jose, Sippel, Martin, Froebel, Ludgar
مصطلحات موضوعية: CDTI in Spain, liquid propellant upper stage, airborne concept, VEGA, Orbspace, Systemanalyse Raumtransport, “CATS”, DLR in Germany, CNES, SPACE TRANSPORTATION, ALDEBARAN, ARIANE 5, “operational responsive space”, military aircraft, SOYUZ, A5ECA version, in-air capturing system, 10kN Lox/Lch4 expander engine
وصف الملف: application/pdf
URL الوصول: https://explore.openaire.eu/search/publication?articleId=od______1640::5646a8d5f77ed6e38849557f97bbb516
https://elib.dlr.de/64520/