Burn Time Correction of Start-Up Transients for CAMUI Type Hybrid Rocket Engine

Burn Time Correction of Start-Up Transients for CAMUI Type Hybrid Rocket Engine

Burn time errors caused by various start-up transient effects have a significant influence on the regression modelling of hybrid rockets. Their influence is especially pronounced in the simulation model of the Cascaded Multi Impinging Jet (CAMUI) hybrid rocket engine. This paper analyses these trans...

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Bibliographic Details
Main Authors: Tor Viscor, Hikaru Isochi, Naoto Adachi, Harunori Nagata
Format: Article
Language:English
Published: MDPI AG 2021-12-01
Series:Aerospace
Subjects:
start-up transient
hybrid rocket
burn time correction
CAMUI
Online Access:https://www.mdpi.com/2226-4310/8/12/385

Internet

https://www.mdpi.com/2226-4310/8/12/385

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