|Table of Contents|

Preliminary analysis on development course of pre-cooling propulsion system(PDF)

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

Issue:
2019年02期
Page:
1-8
Research Field:
专论与综述
Publishing date:

Info

Title:
Preliminary analysis on development course of pre-cooling propulsion system
Author(s):
MA Haibo;  ZHANG Mengzheng
(Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)
Keywords:
pre-cooling propulsion system;  SABRE;  combined engine;  development course
PACS:
V439
DOI:
-
Abstract:
Pre-cooling propulsion system is a hotspot in the field of hypersonic velocity, and is the ideal scheme for the first stage of reusable TSTO vehicle and near space hypersonic launch platform.The development course of pre-cooling propulsion system was reviewed, the typical scheme and research results of each stage were briefly introduced, the evolution process and possible cause were analyzed, and the difference between the principles of the SABRE series was emphasized.The analysis indicates that the main purpose for evolution is to improve pre-cooling efficiency of air, reduce fuel consumption of cooling process and improve comprehensive performance of propulsion system.The current research has shifted from the liquefaction cycle to deep-cooling cycle, and then to the moderate cooling concept represented by SABRE4.Combining with current technical, enhance system feasibility and expedite the transformation from theoretical research to experimental verification under the premise of maximizing the performance of system.

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Last Update: 2019-04-30