Výsledky vyhledávání - "飛行後解析"

Autor: Kato, Sumio, Okuyama, Keiichi, Yamada, Tetsuya

Publikováno v: 宇宙航空研究開発機構研究開発報告: USERS REVカプセルの開発研究および飛行後解析 = JAXA Research and Development Report: Research and Development of USERS REV Capsule and its Post-flight Analysis. :31-54

A computer code for charring ablation and thermal response analysis has been developed for simulation of one-dimensional transient thermal behavior of multi-layer stack of isotropic charring ablation materials used for re-entry capsules. A mathematic

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::1b8bb5d840d7aa8e8359a6c53b9c03e1
http://id.nii.ac.jp/1696/00002314/

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Design and post-flight analysis of REV thermal protection system

Autor: Kato, Sumio, Kanno, Yoshitsugu, Okuyama, Keiichi, Uegaki, Eiichi, Yamada, Tetsuya, Suzuki, Toshiyuki

The re-entry capsule USERS/REV was successfully recovered in May 2003. REV has a heat shield system to protect inner equipments against the severe heating environment during the re-entry. The heat shield system is mainly made of three kinds of layers

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2060c4af55f2565e808c2fd80b69b6a3
http://id.nii.ac.jp/1696/00002316/

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Reproduction of the reentry flight environment based on the USERS capsule flight data

Autor: Yamada, Tetsuya, Ishii, Nobuaki, Matsuda, Seiji

In the final phase of the USERS mission, the REV capsule with orbital experiment samples made a reentry flight from the low earth orbit and was successfully recovered on the sea. Because the USERS REV capsule is the first domestic reentry capsule dev

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ed33ec1a9c2885d6ef94bbfca9fcf2a3
http://id.nii.ac.jp/1696/00002312/

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H-2Aロケット航法誘導系の概要と高機能化に関する一考察

Autor: Mugitani, Takashi, Yokota, Kiyomi

Publikováno v: 平成14年度アストロダイナミクスシンポジウム:講演後刷り集 = ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers. :85-89

H-2Aロケットの航法・誘導系について、その概要(構成、H-2からの変更点など)、試験機1号機についてのフライト結果を紹介するとともに、将来的な高機能化(GPSとの複合化)の1案について考

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3de23229e63a1df86d60feae64bb1a74
http://id.nii.ac.jp/1696/00007771/

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H-2Aロケット制御系の解析評価

Autor: Suzuki, Hideto, Nishihira, Shintaro, Ikeda, Yoshiki, Matsuda, Rika, Nakagawa, Hirofumi, Hattori, Kazue

Publikováno v: 平成14年度アストロダイナミクスシンポジウム:講演後刷り集 = ISAS Proceedings of 12th Workshop on Astrodynamics and Flight Mechanics 2002: A Collection of Technical Papers. :73-78

H-2Aロケットは2001年8月初号機の打上に成功した。H-2Aは高さ約50メートル質量約300トンの日本最大のロケットである。その姿勢制御系は急激に変化する機体特性や構造の柔軟性、液体燃料�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::027c7c21b5b20d411f3301db0e9ea6b7
http://id.nii.ac.jp/1696/00007769/

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Weather monitoring for NEXST-1 flight experiment

Autor: Kawakami, Hiroki, Matayoshi, Naoki, Murakami, Yoshitaka

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1469

独立行政法人航空宇宙技術研究所により豪州ウーメラで実施された小型超音速実験機の第1回飛行実験では、主に実験機装備品の制限と飛行安全上の要求により、射点付近の地表面から計

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4204f456196514e79d3102e7aae1eb85
http://id.nii.ac.jp/1696/00042976/

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