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) |
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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 |
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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