Paper
15 February 2022 Reliability enhancement of the launch vehicle utilization system with the estimation of propellant residual mass
Jinjie Liu, Puhua Wang, Peng Yu
Author Affiliations +
Proceedings Volume 12166, Seventh Asia Pacific Conference on Optics Manufacture and 2021 International Forum of Young Scientists on Advanced Optical Manufacturing (APCOM and YSAOM 2021); 121665M (2022) https://doi.org/10.1117/12.2617560
Event: Seventh Asia Pacific Conference on Optics Manufacture and 2021 International Forum of Young Scientists on Advanced Optical Manufacturing (APCOM and YSAOM 2021), 2021, Hong Kong, Hong Kong
Abstract
A window adaptation linear estimation method of propellant mass is designed, to provide the correct propellant mass input for the utilization system in a variety of malfunction modes, and improve malfunction tolerance. In this way the utilization system can adjust the liquid oxygen control valve according to the predetermined adjustment scheme, amend the mixture ratio of the two propellants close to the theoretical value, and reduce the amount of remaining propellant that cannot be utilized due to the engine mixture ratio errors. And then the delivery capacity of the launch vehicle can be improved.
© (2022) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Jinjie Liu, Puhua Wang, and Peng Yu "Reliability enhancement of the launch vehicle utilization system with the estimation of propellant residual mass", Proc. SPIE 12166, Seventh Asia Pacific Conference on Optics Manufacture and 2021 International Forum of Young Scientists on Advanced Optical Manufacturing (APCOM and YSAOM 2021), 121665M (15 February 2022); https://doi.org/10.1117/12.2617560
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KEYWORDS
Liquids

Rockets

Failure analysis

Data analysis

Error analysis

Oxygen

Reliability

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