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...
Gorde:
| Egile Nagusiak: | , , |
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| Formatua: | Artigo |
| Hizkuntza: | Inglês |
| Argitaratua: |
Wiley
2016-01-01
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| Saila: | International Journal of Aerospace Engineering |
| Sarrera elektronikoa: | http://dx.doi.org/10.1155/2016/3765796 |
| Etiketak: |
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