Slow-Burn Ammonium Perchlorate Propellants with Oxamide: Burn Rate Model, Testing, and Applications
Low-thrust long-burn-time solid rocket motors may be useful as propulsion for small, fast, uncrewed aerial vehicles. These motors require a slow-burning propellant that can operate at unusually low chamber pressures (0.3-2 MPa). Slow-burn propellants were developed using ammonium perchlorate oxidize...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics (AIAA),
2021-06-15T18:18:27Z.
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| Subjects: | |
| Online Access: | Get fulltext |