|Table of Contents|

Discussion about work modal of RBCC power system(PDF)

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

Issue:
2015年02期
Page:
1-6
Research Field:
专论与综述
Publishing date:

Info

Title:
Discussion about work modal of RBCC power system
Author(s):
ZHANG Meng-zheng ZHANG Mei YAN Jun-feng Lü Qi-wei
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
RBCC work modal modal conversion development
PACS:
V434-34
DOI:
-
Abstract:
The manifold work modal of the rocket based combined cycle (RBCC) power system is its leading difference from other power engines. The RBCC power system solution formed by different work modal and engine configuration is the developmental route of RBCC power system, which can satisfy the needs of specific flight mission. The smooth conversion of diverse work modals is the essential need of spacecraft safe work. The intensive research of modal characteristics, technical issues in modal conversion and resolving method is the base of RBCC power system development, and has the important function of shepherding the key technique development. The purpose of developing RBCC power system is to make full use of the advantages of ramjet and rocket engine, remedy the function disfigurement and performance deficiency of LRE or ramjet. The way rests with combination of ripe technology and national demand.

References:

[1]李斌, 张蒙正. 基于火箭/冲压组合的临近空间高速飞行器动力系统方案及面临的挑战[C]. 863-705技术论坛, 长沙: 2008.
[2]张蒙正, 李斌, 王君, 等. 关于动力系统的一点思考[J]. 火箭推进, 2013, 39(1): 1-7.
[3]JOHN E B, JOHN R O, JON G W. Concept assessment of a hydrocarbon fueled RBCC-powered military space plane [R]. USA: AIAA, 2004
[4]SIEBENHAAR A, BUJMAN M J. The Strutjet engine: the overlooked option for space launch, AIAA 95-3124[R]. USA: AIAA, 1995.

[5]JASON E Q. ISTAR: project status and ground test engine design, AIAA 2003-5235[R]. USA: AIAA, 2003.

[6]MELVIN J B, ADMAM S. Combined cycle propulsion: aerojet innovations for practical hypersonic vehicles, AIAA 2011-2397[R]. USA: AIAA, 2011.
[7]SADATAKE T, TETSUO H. Sea-level static tests of a rocket-ramjet combined cycle engine model, AIAA 2007- 5389[R]. USA: AIAA, 2007.
[8]THOMaS M, KRIVANEK J M, ROCHE J P. Affordable flight demonstration of the GTX Air-Breathing SSTO vehicle concept, NASA/TM-2003-212315[R]. USA: NASA/ TM, 2003.
[9]黄生洪, 何洪庆, 何国强. 构型及二次燃烧对RBCC引射模态推力性能的影响[J]. 空气动力学学报, 2005, 23(2):139-143.

Memo

Memo:
-
Last Update: 1900-01-01