Liquid rocket pressurized gas feed systems: Coefficient of discharge (Cd) application-Reference-Cited by-同舟云学术

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Liquid rocket pressurized gas feed systems: Coefficient of discharge (Cd) application

Published:2023 Issue: Volume: Page:
ISSN:0094-243X
Container-title:MACHINE LEARNING AND INFORMATION PROCESSING: PROCEEDINGS OF ICMLIP 2023
language:
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Author:

Mahendra Faishol Luthfy,Hakim Arif Nur,Tahdi Hudoro,Priyadana Ikhwannuary Raditya,Rohman Taufiqur,Moranova Starida

Publisher

AIP Publishing

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0181484

Reference11 articles.

1. ANALISIS KINERJA ENJIN ROKET CAIR ECX1000H2-3

2. A. N. Hakim, H. Tahdi, F. L. Mahendra, “Implementation of Simple Throttling for Liquid Rocket Engine ECX1000H2-4,” 6th International Conference on Science and Technology (Yogyakarta, 2020).

3. Determining the Coefficient of Discharge for a Draining Container

4. Liquid Propulsion: Propellant Feed System Design

5. G.P. Blair, H. B. Lau et al., “Coefficients of Discharge at The Aperatures of Engines,” SAE Technical Paper Series (2018), 952138.

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