@inproceedings{e2daa94bff1a402981efa3752a590a53,
title = "Experimental investigation on a two-phase pulse detonation rocket engine with solenoid valve",
abstract = "In order to increase the operation frequency of a pulse detonation rocket engine (PDRE), a PDRE mockup with solenoid valve was designed whose diameter and length are 30mm and 1000mm respectively. The mockup was performed with liquid C10H21 as fuel, compressed oxygen as oxidizer and nitrogen as purge gas. The PDRE mockup can steadily operate at the frequency of 20~30Hz after taking such measures as selecting high-speed large flow solenoids, heating the fuel and assembling Shchelkin spiral. While the operation frequency is 30Hz, the peak value of detonation wave pressure is 2.2 MPa. The time-averaged thrust of PDRE increases almost linearly with the operation frequency.",
author = "Wang, {Yu Qian} and Wei Fan and Yan, {Chuan Jun} and Li, {Jian Ling}",
year = "2009",
language = "英语",
isbn = "9781563479694",
series = "47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition",
booktitle = "47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition",
note = "47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ; Conference date: 05-01-2009 Through 08-01-2009",
}