Research Article
Multidisciplinary Design Optimization and Analysis of Hydrazine Monopropellant Propulsion System
Table 1
NH3 decomposition and Adiabatic temperature.
| NH3 decomposition
percent | 0% | 20% | 40% | 60% | 80% | 100% |
| | Adiabatic temp. (K) | 1659 | 1501 | 1342 | 1183 | 1023 | 863.1 |
| | Kesten temp. (K) | 1420 | 1306 | 1193 | 1080 | 966.2 | 852.8 |
| | Molecular mass | 19.2 | 16.55 | 14.54 | 12.97 | 11.71 | 10.67 |
| | 1.169 | 1.203 | 1.24 | 1.278 | 1.318 | 1.361 |
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