Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
Kakuda Branch Office, National Aerospace Laboratory(NAL)
National Space Development Agency of Japan(NASDA)
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所報告
雑誌名(英)
Technical Report of National Aerospace Laboratory TR-638
巻
638
ページ
18
発行年
1980-11
抄録（英）
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.
Prediction of the Maximum Force Acting on the Load Cell and Thrust Transient during Rocket Motor Firing Tests
naltr00638.pdf
(1.29MB)
