|Table of Contents|

Discussion on some problems of reusable liquid-propellant engine(PDF)

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

Issue:
2019年04期
Page:
9-15
Research Field:
专论与综述
Publishing date:

Info

Title:
Discussion on some problems of reusable liquid-propellant engine
Author(s):
ZHANG MengzhengZHANG Mei
(Xi’an Aerospace Propulsion Institute,Xi’an 710100,China)
Keywords:
launch vehicle reusable liquid-propellant rocket engine combined cycle engine
PACS:
V434
DOI:
-
Abstract:
Reusable is the important path to reduce the cost of launch vehicle.Reusable of liquid-propellant engine is the key technology and the first problem to be solved.The main development of reusable launch vehicle’s engine is the reusable and low cost liquid-propellant rocket engine and the air-breathed combined cycle engine of the horizontal takeoff-vertical landing vehicle’s first stage engine.The reusable of liquid-propellant rocket engine must innovate design idea,including design method,propellant,material,proper use of ability,manufacture technology and maintaince.The horizontal takeoff-vertical landing vehicle based on combined cycle engine is an important approach to decrease transportation cost and is also an important developing trend for resuable lauch vehicle.Inspired by the reusable design concept of aircraft engine,reusable design idea must be considered in scheme and key technique research stage.

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Last Update: 2019-08-31