Monte Carlo Uncertainty Quantification Using Quasi-1D SRM Ballistic Model
Compactness, reliability, readiness, and construction simplicity of solid rocket motors make them very appealing for commercial launcher missions and embarked systems. Solid propulsion grants high thrust-to-weight ratio, high volumetric specific impulse, and a Technology Readiness Level of 9. Howeve...
שמור ב:
| Principais autores: | , , |
|---|---|
| פורמט: | Artigo |
| שפה: | Inglês |
| יצא לאור: |
Wiley
2016-01-01
|
| סדרה: | International Journal of Aerospace Engineering |
| גישה מקוונת: | http://dx.doi.org/10.1155/2016/3765796 |
| תגים: |
אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!
|