The thermodynamic model of a solid-fuel rocket engine taking into account heat loss-Reference-Cited by-同舟云学术

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The thermodynamic model of a solid-fuel rocket engine taking into account heat loss

Published:2024-06-25 Issue: Volume: Page:
ISSN:2524-7905
Container-title:JMST Advances
language:en
Short-container-title:JMST Adv.

Author:

Phon Nguyen Duy,Van Bien Vo,Phu Nguyen Minh,Dung Nguyen Thai,Le Thai Minh^ORCID

Publisher

Springer Science and Business Media LLC

Link

https://link.springer.com/content/pdf/10.1007/s42791-024-00080-2.pdf

Reference36 articles.

1. P. T. Phiet, Theory of rocket engines, Military Technical academy, Hanoi, Vietnam (1995)

2. P. George Sutton, Rocket Propulsion Elements, 7th Edition, Wiley-Interscience (2000)

3. L.S. Tung et al, Calculation and design of solid fuel rocket engine, Military Institute of Science and Technology, Hanoi, Vietnam (2013)

4. N.V. Giao, Technology for the production of propellant and rocket fuel, Military Technical academy, Hanoi, Vietnam (1999)

5. R.D. Fisher, China’s Emerging 5th Generation Air-to-Air Missiles (Recommended) (IASC, Washington, 2008)

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