Orbital dynamics of magnetoplasma sail

Material type: 規格・テクニカルリポート類

Author: 山川, 宏ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-31

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: 出版タイプ： NAThe orbital dynamics of magnetoplasma sail (MPS) is investigated focusing on the required acceleration for escape from the solar system. One ...

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: 規格・テクニカルリポート類
Title: Orbital dynamics of magnetoplasma sail
Author/Editor: 山川, 宏
Yamakawa, Hiroshi
Author Heading: Yamakawa, Hiroshi
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-31
Publication Date (W3CDTF): 2006
Periodical title: 宇宙航空研究開発機構研究開発報告: 磁気プラズマセイルの推力発生メカニズムの解明 = JAXA Research and Development Report: Elucidation of Thrust Generation Mechanism of Magnetic Sail
No. or year of volume/issue: JAXA-RR-05-014
Volume: JAXA-RR-05-014
Pages: 51-56
ISSN (Periodical Title): ISSN : 1349-1113
Subject Heading: 電磁プラズマセイル
MPS
推力
推進
加速
動径加速度
数学的解析
運動方程式
軌道力学
逃避条件
角運動量
magnetoplasma sail
thrust
propulsion
acceleration
radial acceleration
mathematical analysis
equation of motion
orbital dynamics
escape condition
angular momentum
Target Audience: 一般
Note (General): 出版タイプ： NA
The orbital dynamics of magnetoplasma sail (MPS) is investigated focusing on the required acceleration for escape from the solar system. One of the main features of the MPS propulsion system is that the thrust in confined to anti-sun direction. This motivates the study of the orbital motion under an outward continuous radial acceleration as a function of the distance from the central body. Two representative cases in terms of the MPS power system are analyzed; one is the constant radial acceleration case, and the other assumes the radial acceleration inversely proportional to the square of the radial distance. The former corresponds to constant power case such as Radioisotope Thermoelectric Generator (RTG) system, while the latter corresponds to the case assuming solar paddle for the MPS power system.
資料番号: AA0049193007
レポート番号: JAXA-RR-05-014
Periodical Title (NCID): AA1192675X
https://ci.nii.ac.jp/ncid/AA1192675X
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