|Table of Contents|

Thinking about RBCC propulsion system(PDF)

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

Issue:
2013年01期
Page:
1-7
Research Field:
专论与综述
Publishing date:

Info

Title:
Thinking about RBCC propulsion system
Author(s):
ZHANG Meng-zheng;  LI Bin;  WANG Jun;  Lü Qi-wei
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
-
PACS:
V434-34
DOI:
-
Abstract:
The development course and trend for the rocket based combined cycle (RBCC) propulsion system are reviewed. The velocity, altitude and other basic characteristics of the RBCC propulsion system are analyzed. A suggestion that the development of the RBCC propulsion system should be devoted to improving the function and performance of LRE and ramjet is proposed. It is found that the integrated design of the RBCC propulsion system and aircraft should be enhanced; the sharing of air intake duct, combustor, tailpipe nozzle and fuel supply system might be considered in the integrated design; the study of key and basic technologies of RBCC propulsion system must be carried out according to the specific aircraft project. The development of high-speed aircraft propulsion system running in the near-earth space should be conducted first to tackle the key technology for the second stage of two-stage-to-orbit propulsion systems.

References:

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