Prediction of the Maximum Force Acting on the Load Cell and Thrust Transient during Rocket Motor Firing Tests

Material type: 文書・図像類

Author: 工藤, 賢司ほか

Publisher: 航空宇宙技術研究所

Publication date: 1980-11

Material Format: Digital

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Note (General)：: An impulse test for a thrust stand was conducted and a mathematical model to simulate the main thrust measurement system was presented in order to pre...

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Material Type: 文書・図像類
Title: Prediction of the Maximum Force Acting on the Load Cell and Thrust Transient during Rocket Motor Firing Tests
Author/Editor: 工藤, 賢司
村上, 淳郎
小室, 智幸
石井, 進一
梶原, 堅一
KUDO, Kenji
MURAKAMI, Atsuo
KOMURO, Tomoyuki
ISHII, Shin-ichi
KAJIWARA, Kenichi
Author Heading: 工藤, 賢司
村上, 淳郎
小室, 智幸
石井, 進一
梶原, 堅一
KUDO, Kenji
MURAKAMI, Atsuo
KOMURO, Tomoyuki
ISHII, Shin-ichi
KAJIWARA, Kenichi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1980-11
Publication Date (W3CDTF): 1980-11
Alternative Title: ロケット地上燃焼実験時のロードセル最大荷重と推力立上り特性の推定
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-638
No. or year of volume/issue: 638
Volume: 638
Pages: 18-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): An impulse test for a thrust stand was conducted and a mathematical model to simulate the main thrust measurement system was presented in order to predict the maximum force acting on the load cell and thrust transient characteristics during rocket motor firing tests. An approximating expression for the maximum force acting on the load cell was obtained from the mathematical model and its results agreed well with experimental values. The prediction of the thrust transient was made by using a mathematical model and four alternative methods, and each of their features and problems was described.
資料番号: NALTR0638000
レポート番号: NAL TR-638
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44893&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44893&item_no=1&attribute_id=31&file_no=1
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