Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels-Reference-Cited by-同舟云学术

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Regression rate model assessed by ballistic reconstruction technique in hybrid rocket engines burning liquefying fuels

Published:2022-08 Issue: Volume:127 Page:107712
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Gallo Giuseppe^ORCID,Savino Raffaele

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Overview and history of hybrid rocket propulsion;Altman,2007

2. Hybrid rocket propulsion systems;Altman,1995

3. Turbulent boundary layer combustion in the hybrid rocket;Marxman;Symp., Int., Combust.,1963

4. Evolutions in ballistic data reconstruction techniques for hybrid rockets;Sicat,2021

5. Novel comprehensive technique for hybrid rocket experimental ballistic data reconstruction;Carmicino;J. Propuls. Power,2018

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1. Effect of pressure, Mg content and AP size on the microscale flame structure of Mg-based propellant;Aerospace Science and Technology;2024-07

2. Effect of swirl intensity variation on combustion characteristics in end-burning hybrid rocket engines;Acta Astronautica;2024-04

3. Fast Reconfiguration Maneuvers of a Micro-satellite Constellation Based on a Hybrid Rocket Engine;Aerotecnica Missili & Spazio;2024-03-13

4. Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate;International Journal of Heat and Mass Transfer;2024-03

5. Regression Rate and Performance Analysis via Ballistic Reconstruction of a small-scale H2O2-based Hybrid Rocket fuelled by Polyvinyl Chloride;Aerospace Science and Technology;2024-03

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