Have a personal or library account? Click to login
Preliminary Design Analysis of Regenerative Cooling for N2O/Alcohol Small Scale Liquid Rocket Engine Cover

Preliminary Design Analysis of Regenerative Cooling for N2O/Alcohol Small Scale Liquid Rocket Engine

Transactions on Aerospace Research
Volume 2018 (2018): Issue 3 (September 2018)
By: Patryk Palej and  Tomasz Palacz  
Open Access
|Sep 2019
DOI: https://doi.org/10.2478/tar-2018-0024 | Journal eISSN: 2545-2835
Journal RSS Feed
Language: English
Page range: 87 - 102
Published on: Sep 4, 2019
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year
Keywords:
liquid rocket engine,
regenerative cooling,
nitrous oxide,
sounding rocket
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other,
Geosciences,
Geosciences, other,
Materials sciences,
Materials sciences, other,
Physics,
Physics, other

© 2019 Patryk Palej, Tomasz Palacz, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Previous articleVolume 2018 (2018): Issue 3 (September 2018)Next article