Direct formulation and quantitative water-flow diagnostic for bi-propellant thruster performance

Chihiro Inoue, Yuki Oishi, Yuto Terauchi, Yu Daimon, Go Fujii, Kaname Kawatsu

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

We present an original formulation predicting the characteristic velocity and specific impulse for bi-propellant thrusters as the straightforward function of injection conditions, propellant combination, and nozzle configuration. The validity is demonstrated by comparing with corresponding combustion test results in the past using NTO and MMH as the propellant under several injector unlike-doublet and triplet configurations. The theoretical formulation deduces a framework for a quantitative cold flow test to predict characteristic velocity. We employ water and dyed water as simulant liquids, which are environmentally friendly and easy to handle, and then, measure the local ratios of mixture and flow rate using an absorbance spectrometer. Density ratio mismatch between hypergolic propellants and water can be reasonably compensated. Combined with chemical equilibrium analysis, we calculate characteristic velocity for a wide range of injection mixture ratios. The validity of the quantitative water-flow diagnostic is also evidenced by comparing the results with those of corresponding combustion tests, indicating that the mixing states of bi-propellant thrusters under combustion can be reproduced using the water-flow diagnostic.

本文言語英語
ホスト出版物のタイトルAIAA Propulsion and Energy 2020 Forum
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ページ1-13
ページ数13
ISBN(印刷版)9781624106026
DOI
出版ステータス出版済み - 2020
イベントAIAA Propulsion and Energy 2020 Forum - Virtual, Online
継続期間: 8 24 20208 28 2020

出版物シリーズ

名前AIAA Propulsion and Energy 2020 Forum

会議

会議AIAA Propulsion and Energy 2020 Forum
CityVirtual, Online
Period8/24/208/28/20

All Science Journal Classification (ASJC) codes

  • エネルギー(全般)
  • 航空宇宙工学
  • 制御およびシステム工学
  • 電子工学および電気工学
  • 機械工学

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