Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1715025 | Acta Astronautica | 2013 | 11 Pages |
Abstract
⺠A code for hybrid rocket unsteady operation and transit fuel regression is developed. ⺠Calculated thrust and chamber wall profile are in good agreement with test data. ⺠New coefficients for regression rate equation are derived. ⺠Regression rate is function of chamber diameter leading to analysis of scale effect.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Fanli Shan, Lingyun Hou, Ying Piao,