Comprehensive Data Reduction for N<sub>2</sub>O/HDPE Hybrid Rocket Motor Performance Evaluation
Static firing tests of a hybrid rocket motor using liquid nitrous oxide (N<sub>2</sub>O) as the oxidizer and high-density polyethylene (HPDE) as the fuel are analyzed using a novel approach to data reduction that allows histories for fuel mass consumption, nozzle throat erosion, characte...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2019-04-01
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| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/6/4/45 |