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Liquid Rocket Propulsion - Evolution and Advancements: Rocket-Based Combined Cycle.

机译：液体火箭推进 - 演变与进步：基于火箭的联合循环。

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摘要

This document on Rocket-Based Combined Cycles discusses history of RBCC, integrated performance analysis, current activities and future prospects.

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Moszee, R.;
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年度 1999
页码 1-49
总页数 49
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Liquid propellant rocket engines; Rocket propulsion; Integrated systems; Performance tests; Liquid rocket fuels; Supercharged ejector ramjet engines; Viewgraphs only; Rene(Rocket engine nozzle ejector);

机译：液体推进剂火箭发动机;火箭推进器;集成系统;性能测试;液体火箭燃料;增压喷射器冲压式喷气发动机;仅视图; Rene（火箭发动机喷嘴喷射器）;

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1. Maximum thrust for the rocket-ejector mode if the hydrogen fueled rocket-based combined cycle engine [J] . Yang Qingchun, Shi Wen, Chang Juntao, International journal of hydrogen energy . 2015,第9期

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2. Experimental Investigation of an Alternative Rocket Configuration for Rocket-Based Combined Cycle Engines [J] . J. Etele, S. Hasegawa, S. Ueda Journal of propulsion and power . 2014,第4期

机译：基于火箭的联合循环发动机的替代火箭构型的实验研究
3. Secondary fuel jet strategies on mixing enhancement performance of rocket-based combined cycle engine [J] . Dai Jian, Huang Chao Acta astronautica . 2021,第Jana期

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4. A User's Primer for Comparative Assessments of All-Rocket and Rocket-Based Combined-Cycle Propulsion Systems for Advanced Earth-to-Orbit Space Transport Applications [C] . William J.D.Escher, Eric H.Hyde, David M.Anderson 31st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 10-12, 1995/San Diego, CA . -1

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5. An Ejector Air Intake Design Method for a Novel Rocket-Based Combined-Cycle Rocket Nozzle [D] . Waung, Timothy S. 2010

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6. A Prospective Study of the Surgical Outcome of Simple Uvulopalatopharyngoplasty (UPPP) UPPP Combined With Genioglossus Advancement or Tongue Base Advancement for Obstructive Sleep Apnea Hypopnea Syndrome Patients With Multilevel Obstruction [O] . Shicai Chen, Song Shi, Yanghui Xia, 2016

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7. Computational Analysis for Rocket-Based Combined-Cycle Systems During Rocket-Only Operation [O] . Yungster S., Steffen C. J. Jr., Smith T. D., 2000

机译：基于火箭的联合循环系统仅火箭运行时的计算分析

Liquid Rocket Propulsion - Evolution and Advancements: Rocket-Based Combined Cycle.

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