Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy-Reference-Cited by-同舟云学术

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Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy

Published:2021-11 Issue: Volume:188 Page:110-120
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Wang Zezhong,Lin Xin^ORCID,Li Fei^ORCID,Peng Jinlong,Liu Yan,Zhang Zelin,Fang Sihan^ORCID,Yu Xilong

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference55 articles.

1. Performance comparison of oxidizer injectors in a 1-kN paraffin-fueled hybrid rocket motor;Bouziane;Aero. Sci. Technol.,2019

2. Integration validation of key components for small sounding rockets;Yun;Aero. Sci. Technol.,2020

3. The nammo nucleus launch: Norwegian hybrid sounding rocket over 100km;Faenza,2019

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

5. Sounding rocket “HEROS” - a low-cost hybrid rocket technology demonstrator;Kobald,2017

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