Review Article
Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines
Table 2
Optimal design and performance of sounding rocket for different propellant combinations.
| | Propellants | ( ) | | Reference | (kN) | | (kg) | (m) | (m) | (s) |
| | HP/PE | |
0.800
| [38] | 24.8 | 8.57 | 339 | 0.42 | 5.01 | 299 | | LOX/HTPB | |
0.852
| [39] | 23.5 | 3.20 | 328 | 0.46 | 5.52 | 219 | | N2O/HTPB | |
0.347
| [40] | 16.2 | 10.92 | 340 | 0.40 | 4.75 | 177 |
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