タイトル | Stress-testing of the throat of a rocket's nozzle |
本文(外部サイト) | http://hdl.handle.net/2060/19690000356 |
著者(英) | Estes, E. G. |
発行日 | 1969-09-01 |
言語 | eng |
内容記述 | Test motor in which high initial pressure can be reduced suddenly provides a method of testing stress effects in the throat of a rockets nozzle. Motors operating pressure is increased to aggravate tensile stresses in a submerged throat. Opposing compression stresses are limited by control of the operating pressure. |
NASA分類 | MECHANICS |
レポートNO | 69B10358 NPO-10311 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/502626 |