原型機飛行試験による航空機用電動推進系の仕様検討

Material type: 文書・図像類

Author: 小林, 宙ほか

Publisher: 宇宙航空研究開発機構(JAXA)

Publication date: 2015-03-13

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: The Japan Aerospace Exploration Agency (JAXA) is planning flight demonstration of an electric propulsion system which is equipped with new functions u...

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: 原型機飛行試験による航空機用電動推進系の仕様検討
Author/Editor: 小林, 宙
飯島, 朋子
西沢, 啓
Kobayashi, Hiroshi
Iijima, Tomoko
Nishizawa, Akira
Author Heading: 小林, 宙
飯島, 朋子
西沢, 啓
Kobayashi, Hiroshi
Iijima, Tomoko
Nishizawa, Akira
Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
Publication Date: 2015-03-13
Publication Date (W3CDTF): 2015-03-13
Alternative Title: Required Specifications of an Electric Propulsion System Based on Flight Test Using a Motor Glider
Periodical title: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum
No. or year of volume/issue: JAXA-RM-14-005
Volume: JAXA-RM-14-005
Pages: 1-7
ISSN (Periodical Title): ISSN : 1349-1121
Text Language Code: jpn
Subject Heading: electric propulsion system
flight test
Target Audience: 一般
Note (General): The Japan Aerospace Exploration Agency (JAXA) is planning flight demonstration of an electric propulsion system which is equipped with new functions using a motor glider on 2014. The new electric propulsion system will be converted form the existing reciprocating engine of motor glider and be installed with motor glider. Prior to the development of the electric propulsion system, flight tests are conducted to acquire performance of JA07TTCECO with original propulsion system. Based on these flight test result, determined specifications of the electric propulsion system for replacing original system are as follows, 1)Take-off Power(max 150s):60kW, 2)Maximum Propeller Speed:2300rpm, 3)Maximum Ambient Temperature:40 C, 4)Maximum Continuous Power:32kW.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA1530008000
レポート番号: JAXA-RM-14-005
Access Restrictions: 限定公開
Periodical Title (NCID): AA11983593
https://ci.nii.ac.jp/ncid/AA11983593
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