Research Article
Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant
Table 5
Comparison of modeling and experimental results for
long grains.
| | Total impulse (N-s) | Peak (MPa) | Peak thrust (kN) |
| | Model with no losses ( long grain) | 1484 | 14.68 | 1.98 | | Model with deposit & losses ( long grain) | 1336 | 14.82 | 1.78 | | Long experimental grain (Test 4) | 970 | 14.89 | 2.13 | | Long experimental grain (Test 5) | 890 | 11.72 | 1.56 |
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