|Table of Contents|

Application of RBCC and TBCC engines to RLVs(PDF)

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

Issue:
2008年03期
Page:
39-43
Research Field:
燃料与推进剂
Publishing date:

Info

Title:
Application of RBCC and TBCC engines to RLVs
Author(s):
Chen Hong1; He Guoqiang2
1 The 41st Institute of the Fourth Academy of CASC，National Key Lab of Combustion， Flow and Thermo—Structure，Xi7an 7 10025，China； 2 College of Astronautics，Noahwestem Polytechnical University，Xi'an 7 10072，China
Keywords:
two-phase reacting flow; combustion chamber; finite rate; EDC; PDF; combustion model
PACS:
V438
DOI:
-
Abstract:
The application of combined airbreathing engines used for the next generation reusable launch vehicle(RLV)was presented．Two-Stage-To—Orbit RLV configurations using corn— bined propulsion systems for both stages were described，and a comparison was made between RBCC and TBCC to analyze their effects on the general performances of RLV．Two recommended RLV configurations were shown consequently．

References:

[1]陈宏．高超飞行器推进系统概念研究[D]．西安：西北工业 大学．2005．
[2]Wagner A，Bouchez M．Integration of a Combined Engine Propulsion System into a SSTO Launcher[R]．AIAA一95— 6044．
[3]Roche J M．Structural Sizing of A 250001b Payload Air— Breathing Launch Vehicle for Single-Stage-To—Orbit． JANNF 25th airbreathing propulsion subcommittee[C]． 37th combustion subcommittee and 1st modeling＆ simulation subcommittee joint meeting，vol(1)．
[4]Roche J M．Preliminary Sizing of Vertical Take-Off Rocket- Based Combined—Cycle Powered Launch Vehicles[C]． JANNF 25th airbreathing propulsion subcommittee，37th combustion subcommittee and 1st modeling＆simulation subcommittee joint meeting，vol(1)．
[5]Hank J M，Franke M E．TSTO Reusable Launch Vehicles Using Airbreathing Propulsion[R]．AIAA 2006--4962．
[6]Caldwell R A，Franke M E．Weight Analysis of Two— Stage-To-Orbit Reusable Launch Vehicles[R]．AIAA 2005—4365．
[7]Kokan T，Olds J R．Aztec：A TSTO Hypersonic Vehicle Concept Utilizing TBCC and HEDM Propulsion Techno— logies[R]．AIAA2004—3728．
[8]8 Andrew M Crocker,Jeffery H Cannon，Dana G Andrews． A Comparison of Horizontal Takeoff RLVS for Next Generation Space Transportation[R]．AIAA 2003—5037．
[9]Culver G．Probabilistic Performance Comparison of RBCC and TBCC—Based Reusable Launch Vehicles with Enhan— eing Technologies[R]．AIAA 2003-5035．

Memo

Memo:
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Last Update: 1900-01-01