Scheme design and assessment of hybrid pump feed system with energy management for throttleable liquid rocket engine

Currently, there is considerable emphasis on the electric pump-fed cycle for liquid engine, primarily due to its design simplicity. However, its development is hindered by the underdeveloped state of power battery technology. Drawing inspiration from hybrid power technology used in electric vehicles and turbochargers, a hybrid pump feed system for throttleable engines is originally proposed as a promising solution. This system integrates the electric motor into the gas generator cycle, with several topologies evaluated. The parallel configuration featuring a mid-motor is selected for its compact structure, efficient power-splitting and energy recovery. Additionally, customized energy management strategies and optimization models are developed to effectively allocate power throughout the operational processes of liquid engines. A comparative analysis of four engine cycles is conducted under the typically variable-thrust mission. The results indicate that attributed to the conservation of turbo-gas and battery energy, the optimized hybrid pump achieves a reduction of 2.39 % compared to the turbopump and 7.15% to the electric pump in total mass. Adaptability assessment further indicates that the mass advantage of the hybrid pump system is more significant during prolonged engine burning and deep throttling. Specific working conditions are found in which the system prefers electric-motor driving or regenerating turbine energy. Although energy-recovery results in the system efficiency decrease, it serves to lower energy demand of battery pack, thus easing the burden on cell thermal management and structural design. This study provides a practical design framework for hybrid pump-fed rocket engines in future variable-thrust missions. • The practical scheme of hybrid pump feed system for liquid engine is originally proposed. • Energy management strategies with respect to throttleable engine mission profile is designed. • A comparison is conducted between the hybrid pump, electric pump, and gas generation cycle. • Long-term firing and prolonged, deep throttling of engine conditions have been found to be effective for the hybrid pump system.

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Publication Details

Journal
Acta Astronautica
Published
2024-10-09
DOI
https://doi.org/10.1016/j.actaastro.2024.10.013
Citations
2
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
2.60
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article

Scheme design and assessment of hybrid pump feed system with energy management for throttleable liquid rocket engine

Jiangning Wang, Guobiao Cai, Xintong Li, Yuanjun Zhang et al.
2 citations
Acta Astronautica
Rocket and propulsion systems research
2.60
article

Scheme design and assessment of hybrid pump feed system with energy management for throttleable liquid rocket engine

Jiangning Wang, Guobiao Cai, Xintong Li, Yuanjun Zhang, Hao Zhu, Hui Tian, Jincheng Wang
article en
2 citations

Abstract

Currently, there is considerable emphasis on the electric pump-fed cycle for liquid engine, primarily due to its design simplicity. However, its development is hindered by the underdeveloped state of power battery technology. Drawing inspiration from hybrid power technology used in electric vehicles and turbochargers, a hybrid pump feed system for throttleable engines is originally proposed as a promising solution. This system integrates the electric motor into the gas generator cycle, with several topologies evaluated. The parallel configuration featuring a mid-motor is selected for its compact structure, efficient power-splitting and energy recovery. Additionally, customized energy management strategies and optimization models are developed to effectively allocate power throughout the operational processes of liquid engines. A comparative analysis of four engine cycles is conducted under the typically variable-thrust mission. The results indicate that attributed to the conservation of turbo-gas and battery energy, the optimized hybrid pump achieves a reduction of 2.39 % compared to the turbopump and 7.15% to the electric pump in total mass. Adaptability assessment further indicates that the mass advantage of the hybrid pump system is more significant during prolonged engine burning and deep throttling. Specific working conditions are found in which the system prefers electric-motor driving or regenerating turbine energy. Although energy-recovery results in the system efficiency decrease, it serves to lower energy demand of battery pack, thus easing the burden on cell thermal management and structural design. This study provides a practical design framework for hybrid pump-fed rocket engines in future variable-thrust missions. • The practical scheme of hybrid pump feed system for liquid engine is originally proposed. • Energy management strategies with respect to throttleable engine mission profile is designed. • A comparison is conducted between the hybrid pump, electric pump, and gas generation cycle. • Long-term firing and prolonged, deep throttling of engine conditions have been found to be effective for the hybrid pump system.

Acta AstronauticaVol. 226
Beihang University (CN)
Affordable and clean energy
Openalex Percentile: Top 8%
Rocket and propulsion systems research
2.60
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