Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber
- DOI
- 10.2514/6.2021-3495
- Published
- 2021-07-28
- Container
- Not recorded
- Publisher
- American Institute of Aeronautics and Astronautics
- Open access
- yes
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Cite this work
BibTeX
@article{allodium:10.2514/6.2021-3495,
title = {Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber},
author = {Elena Quero Granado and Jouke Hijlkema and Jean-Yves Lestrade and Jerome Anthoine},
year = {2021},
doi = {10.2514/6.2021-3495},
url = {https://doi.org/10.2514/6.2021-3495}
}RIS
TY - JOUR TI - Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber AU - Elena Quero Granado AU - Jouke Hijlkema AU - Jean-Yves Lestrade AU - Jerome Anthoine PY - 2021 DO - 10.2514/6.2021-3495 UR - https://doi.org/10.2514/6.2021-3495 ER -
APA
Granado, E. Q., Hijlkema, J., Lestrade, J., & Anthoine, J. (2021). Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber. https://doi.org/10.2514/6.2021-3495
Source records
- hal · retrieved 2026-09-27T08:52:05.444Z