Flow feedback control based on variable area cavitating venturi and its application in hybrid rocket motors-Reference-Cited by-同舟云学术

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Flow feedback control based on variable area cavitating venturi and its application in hybrid rocket motors

Published:2023-10 Issue: Volume:211 Page:238-248
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Tan Guang,Tian Hui^ORCID,Gu Xiaoming,Meng Xiangyu,Wei Tianfang,Zhang Yuanjun,Cai Guobiao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Development and application of hybrid rocket motor technology: overview and prospect;Guobiao;J. Propuls. Technol.,2012

2. Throttleable Hybrid Engine for Planetary Soft Landing;Parissenti,2011

3. Variable thrust, multiple start hybrid motor solutions for missile and space applications;Austin,2010

4. Early developments in hybrid propulsion technology at the air force rocket propulsion laboratory;Mead,1995

5. Hybrid rocket development history;Altman,1991

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1. Research on Virtual Prototype and Digital Test Method of Pump-Fed Propulsion System;International Journal of Aeronautical and Space Sciences;2024-09-14

2. Transient Effects by Pintle Motion in Cavitating Venturi Tube for Throttled Bipropellant Thruster;Acta Astronautica;2024-09

3. Experimental and numerical investigation on thermochemical erosion and mechanical erosion of carbon-based nozzles in hybrid rocket motors;Aerospace Science and Technology;2024-05

4. Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units;Aerospace;2024-03-28

5. Numerical simulation on the enhancement mechanism of the distinctive division baffle on the performance of a Venturi for process intensification;Journal of Water Process Engineering;2024-01

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