Experimental Study on the Mass Flow Rate of the Self-Pressurizing Propellants in the Rocket Injector

High vapor pressure propellants such as nitrous oxide are widely used in experimental hybrid and liquid rockets as they can be used in a self-pressurization mode, eliminating the need for external pressurization or pumps and simplifying the design of the rocket system. This approach causes the two-p...

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Bibliographic Details
Main Authors: Tomasz Palacz, Jacek Cieślik
Format: article
Language:EN
Published: MDPI AG 2021
Subjects:
Online Access:https://doaj.org/article/9874cc05e0e6409bafc95d6a2106cf9d
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