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The Study on High-Precision Flow Rate Prediction for LOX/Ethanol Gas Generator
- Source :
- 令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022.
- Publication Year :
- 2023
- Publisher :
- 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), 2023.
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Abstract
- 令和4年度宇宙輸送シンポジウム(2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)) , 相模原市, 神奈川県<br />Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan<br />In this paper, describe a method of prediction for gas generator throttled combustion tests. In addition to the conventional method, the injector Cd was set small based on past test results. As a result, the LOX flow rate error at 70% throttle was improved from 10% to 1.3%. In addition, for flight operation, the propellant orifice diameter was examined for the feed-line resistance of the control valves.<br />資料番号: SA6000184027<br />STCP-2022-027
- Subjects :
- Throttling
Pressure Loss
Gas Generator
Flow Rate
Subjects
Details
- Language :
- Japanese
- Database :
- OpenAIRE
- Journal :
- 令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022
- Accession number :
- edsair.jairo.........16be24e051e6abb1774b2d7c0d7e0269