Rocket Engine with Continuous Film Detonation of Liquid Fuel


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

详细

It was experimentally proven for the first time that it is possible to perform continuous detonation combustion of a film of a liquid fuel in the annular combustor of a demonstrator of a liquid-fuel detonation rocket engine. Firing tests revealed a near-limit mode of longitudinally pulsating film detonation and modes of continuous spinning film detonation with one and two detonation waves circulating within the annular gap of the combustor.

作者简介

S. Frolov

Semenov Institute of Chemical Physics; National Research Nuclear University (MEPhI); Scientific Research Institute for System Analysis

编辑信件的主要联系方式.
Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991; Moscow, 115409; Moscow, 117218

I. Shamshin

Semenov Institute of Chemical Physics; National Research Nuclear University (MEPhI); Scientific Research Institute for System Analysis

Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991; Moscow, 115409; Moscow, 117218

V. Aksenov

Semenov Institute of Chemical Physics; National Research Nuclear University (MEPhI)

Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991; Moscow, 115409

I. Sadykov

Semenov Institute of Chemical Physics

Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991

P. Gusev

Semenov Institute of Chemical Physics; Joint Institute of High Temperatures

Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991; Moscow, 125412

V. Zelenskii

Baikov Institute of Metallurgy and Materials Science

Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991

E. Evstratov

Baikov Institute of Metallurgy and Materials Science

Email: smfrol@chph.ras.ru
俄罗斯联邦, Moscow, 119991

M. Alymov

Merzhanov Institute of Structural Macrokinetics and Problems of Materials Science

Email: smfrol@chph.ras.ru
俄罗斯联邦, Chernogolovka, Moscow oblast, 142432

补充文件

附件文件
动作
1. JATS XML

版权所有 © Pleiades Publishing, Ltd., 2018