A comprehensive fluid–solid coupling dynamic simulation for spatiotemporal distribution of regression rate in hybrid rocket motors-Reference-Cited by-同舟云学术

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A comprehensive fluid–solid coupling dynamic simulation for spatiotemporal distribution of regression rate in hybrid rocket motors

Published:2024-02 Issue: Volume: Page:
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

WEI Tianfang,CAI Guobiao,TIAN Hui,MENG Xiangyu,JIANG Xianzhu,GU Xiaoming

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference33 articles.

1. Kuo KK, Chiaverini MJ. Fundamentals of hybrid rocket combustion and propulsion. Reston: AIAA; 2007.

2. Hybrid rocket propulsion technology for space transportation revisited - propellant solutions and challenges;Okninski;FirePhysChem,2021

3. The regolith rocket—A hybrid rocket using lunar resources;Stoll;Acta Astronaut,2021

4. Development of the ILR-33 “Amber” sounding rocket for microgravity experimentation;Marciniak;Aerosp Sci Technol,2018

5. Demonstration of tethered hovering flight of HTTP-3AT hybrid rocket;Wei;Acta Astronaut,2022

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