|Table of Contents|

Research progress of liquid propellant development for RBCC engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2022年06期
Page:
101-112
Research Field:
目次
Publishing date:

Info

Title:
Research progress of liquid propellant development for RBCC engine
Author(s):
WANG Jingqi;  WANG Chenggang;  CHEN Xuejiao;  MA Liya;  JIANG Rongpei
(Aerospace Liquid Propellant Research Center, Beijing Institute of Aerospace Testing Technology, Beijing 100074, China)
Keywords:
rocket based combined cycle liquid propellant hydrocarbon fuel green propellant nitrogen tetroxide hydrogen peroxide
PACS:
V511
DOI:
-
Abstract:
Combined with the development requirements of RBCC engine, the latest research of the fuels for air-breathing mode and the propellants for all-rocket propulsion system with the aspects of performance and usability is discussed, including endothermic hydrocarbon fuel, high-density endothermic hydrocarbon fuel, nitrogen tetroxide/green hypergolic fuel and hydrogen peroxide/hydrocarbon fuel.In order to meet the long-term storage requirements of propellant for RBCC system, it is necessary to develop the hydrocarbon fuels with both high density and strong heat sink for the air-breathing mode. Correspondingly, the new green hypergolic fuels should be developed for the rocket mode, which can spontaneously have the low ignition delay with nitrogen tetroxide and the high specific impulse.Meanwhile, the safety and storage stability of hydrogen peroxide should be promoted with a reliable safety control method.In view of the long-term storage and maintenance-free requirements of RBCC system, the existing propellant schemes still need to carry out key technological breakthroughs in performance improvement, engineering applicability, system matching and other aspects.

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