| Item type |
紀要論文 / Departmental Bulletin Paper(1) |
| 公開日 |
2015-03-26 |
| タイトル |
|
|
タイトル |
Destruction Test of Small Scaled Solid Propellant Motors |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_6501 |
|
資源タイプ |
departmental bulletin paper |
| 著者 |
HINADA, Motoki
AKIBA, Ryojiro
KISHI, Teruo
MATOGAWA, Yasunori
TSUKAMOTO, Shigeki
|
| 出版者 |
|
|
出版者 |
宇宙科学研究所 |
| 出版者(英) |
|
|
出版者 |
Institute of Space and Astronautical Science |
| 書誌情報 |
en : The Institute of Space and Astronautical Science report
巻 620,
p. 1-20,
発行日 1986-11
|
| 抄録(英) |
|
|
内容記述タイプ |
Other |
|
内容記述 |
Destruction tests have been carried out on the ground by using three small scaled motors of solid propellant with a pair of destruction devices of V-shaped charge type. Each motor has the size of about 1/10 of the rear segment of one third of the 1st stage of Mu-3C that is a three staged and all solid propellant satellite launcher, developed by ISAS. Destruction devices in these tests are roughly the same in function and installation as those for Mu-3C. Several interesting results have been obtained on breakup characteristics of motor, such as mode of destruction, shapes of fragments of propellant and hardware, scattering distribution of them, shock load undergone by motor and surrounding overpressure. These results are expected to be useful for prediction of breakup characteristics of Mu-3C due to V-shaped charges. |
| ISSN |
|
|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0285-6808 |
| 書誌レコードID |
|
|
収録物識別子タイプ |
NCID |
|
収録物識別子 |
AA10632072 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA0035009000 |