Effect of multi-location swirl injection on the performance of hybrid rocket motor-Reference-Cited by-同舟云学术

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Effect of multi-location swirl injection on the performance of hybrid rocket motor

Published:2020-11 Issue: Volume:176 Page:111-123
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Vignesh Bala,Kumar Rajiv

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. Hybrid propellant rockets;Sutton,2000

2. Overview and history of hybrid rocket propulsion;Altman,2006

3. Approaches to low fuel regression rate in hybrid rocket engines;Pastrone;Int. J. Aerosp. Eng.,2012

4. Hybrid rocket engines: the benefits and prospects;Davydenko;Aero. Sci. Technol.,2007

5. Flame propagation in weightlessness above the burning surface of material;Tyurenkova;Acta Astronaut.,2019

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1. Effect on the Performance of a Hybrid Rocket using AP in the PVC and HTPB-Based Hybrid Fuel;FirePhysChem;2024-08

2. Performance estimation of hybrid rocket by varying the flow rate at multi-location swirl injector;FirePhysChem;2024-08

3. Combustion Characteristics of Vat-Photopolymerized Fuels with a Spiral Star Port for Hybrid Propulsion;Langmuir;2024-05-14

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

5. Performance Estimation by Varying the Grain Port Alignment Position in a Hybrid Rocket Motor;Defence Science Journal;2024-03-26

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