Abstract
A transient, two-dimensional computer code describing the simultaneous process of thermochemical ablation and mechanical erosion is employed to predict the erosion phenomena of MXBE-350. The results generated from this code were compared with the experimental data performed by FMC on SSRM facility. Reasonable agreement were found between the numerical prediction and the measured results.
| Original language | English (US) |
|---|---|
| State | Published - 1995 |
| Event | 33rd Aerospace Sciences Meeting and Exhibit, 1995 - Reno, United States Duration: Jan 9 1995 → Jan 12 1995 |
Other
| Other | 33rd Aerospace Sciences Meeting and Exhibit, 1995 |
|---|---|
| Country/Territory | United States |
| City | Reno |
| Period | 1/9/95 → 1/12/95 |
All Science Journal Classification (ASJC) codes
- Space and Planetary Science
- Aerospace Engineering
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