多目的プラットフォームの振動解析

Material type: 文書・図像類

Author: 塙, 武敏ほか

Publisher: 航空宇宙技術研究所

Publication date: 1984-04

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: This paper presents some results of the vibration analysis for simplified models of a multipurpose geostationary platform. The analysis approach is ba...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which Institutional Repositories DataBase(IRDB)(Institutional Repository) is linked at the site of Institutional Repositories DataBase(IRDB)(Institutional Repository).
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: 多目的プラットフォームの振動解析
Author/Editor: 塙, 武敏
狼, 嘉彰
中井, 暎一
只川, 嗣朗
HANAWA, Taketoshi
OOKAMI, Yoshiaki
NAKAI, Eiichi
TADAKAWA, Tsuguo
Author Heading: 塙, 武敏
狼, 嘉彰
中井, 暎一
只川, 嗣朗
HANAWA, Taketoshi
OOKAMI, Yoshiaki
NAKAI, Eiichi
TADAKAWA, Tsuguo
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1984-04
Publication Date (W3CDTF): 1984-04
Alternative Title: Vibration Analysis of a Multipurpose Platform
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-803
No. or year of volume/issue: 803
Volume: 803
Pages: 40-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): This paper presents some results of the vibration analysis for simplified models of a multipurpose geostationary platform. The analysis approach is based on the energy method that has been applied by one of authors using assumed mode functions for the purpose of analysing aircraft vibration problems. For the detailed analysis, the finite element method is widely used, but in a preliminary analysis the method described here is also useful since it is computationally tractable and easy to handle although there are constraints on the configuration complexity. The paper consists of two parts. The first part describes a mission model of the proposed platform containing six missions of communication and broadcasting. Launch sequences and deployments of the platform, and mass and inertia properties of the constitutent modules are briefly explained. The second part presents the analysis procedure, together with the simplifing assumptions, and the main results. The analyses are performed not only for the final platform of cross type and T-letter configuration but also for the interim stages of construction. The results are shown in figures with numerical tables.
資料番号: NALTR0803000
レポート番号: NAL TR-803
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ