Výsledky vyhledávání - "Tomoko IRIKADO"

Numerical Analysis on Aerodynamic Characteristics of Advanced Solid Rocket

Autor: Keiichiro Fujimoto, Moriyasu Fukuzoe, Satoshi Nonaka, Eiji Shima, Tomoko Irikado, Kazuto Kuzuu, Keiichi Kitamura

Publikováno v: AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 10:1-10

The Advanced Solid Rocket (currently Epsilon Launch Vehicle) is under the development by JAXA (Japan Aerospace Exploration Agency). In this study, using our cutting-edge CFD technology, we carried out numerical analysis on the aerodynamic characteris

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a7389b9529552617425ec925c8d43495
https://doi.org/10.2322/astj.10.1

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Wind Tunnel Tests on Aerodynamic Characteristics of Advanced Solid Rocket

Autor: Eiji Shima, Moriyasu Fukuzoe, Keiichiro Fujimoto, Keiichi Kitamura, Satoshi Nonaka, Tomoko Irikado

Publikováno v: AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 9:9-14

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a82b6659d04366112ff3bafe0c0483dc
https://doi.org/10.2322/astj.9.9

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PSP measurements of the pressure fields over the a complicated model configuration

Autor: Kozo Fujii, Nobuyoshi Fujimatu, Tomoko Irikado, Kiyoshi Sato, Hirofumi Ouchi

Publikováno v: Journal of the Visualization Society of Japan. 24:379-382

Surface pressure of a complicated space shuttle type model has been measured by using the pressure sensitive paint (PSP) in the ISAS/JAXA transonic large-scale wind tunnel. A new automatic marker detection method is has been developed so that all mar

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::53ed5d4a19546864a1919cad9af96219
https://doi.org/10.3154/jvs.24.supplement1_379

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BepiColombo/MMO Thermal Test Model Testing

Autor: Akira Okamoto, Shun Okazaki, Fuyuko Fukuyoshi, Tomoko Irikado, Hiroyuki Ogawa, Naoko Iwata, Tsutomu Yamazaki

Publikováno v: Scopus-Elsevier

Lessons learned and results from BepiColombo/Mercury Magnetospheric Orbiter (MMO) thermal test model testing are presented. The MMO Thermal Test Model (TTM) was elaborately tested in four Thermal Balance Tests (TBTs): TBT with a 1 solar constant simu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e11b1c5f0d2dea2189fb1c8bad5ab133
https://doi.org/10.2514/6.2011-5189

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Investigation of Aerodynamic Characteristics of the Tilted Toroidal Ballute System

Autor: Wataru Enya, Gento Ichikawa, Tomoko Irikado, Takashi Abe, Hirotaka Otsu

Publikováno v: 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.

The aerodynamic characteristics of the reentry vehicle system with the tilted toroidal ballute are investigated using CFD analyses and supersonic wind tunnel experiments. The wind tunnel experiments were performed using ISAS/JAXA supersonic wind tunn

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::3cc1599b37632bb2c9786b75917111a0
https://doi.org/10.2514/6.2009-729

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A Study of Fuselage Configurations for Reusable Launch Vehicles

Autor: Yasuhiro Tani, Yoshifumi Inatani, Takuro Ishida, Shigeru Aso, Tomoko Irikado

Publikováno v: 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition.

A numerical study on the fuselage configurations of reusable launch vehicles (RLVs) has been conducted. The models for the numerical simulations were the models which wind tunnel experiments were conducted previously (named in this paper as triangle

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::43392d856b74af8544295e2d43230058
https://doi.org/10.2514/6.2009-906

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