@inproceedings{e1740e2a711d42cf949e9b9a623c62dd,
title = "Experimental tests of throttleable H2O2/PE hybrid rocket motors",
abstract = "A series of throttleable hybrid rocket motors were developed to assess the throttling capability of hybrid rocket motors. The motors used polyethylene (PE) as solid fuel and 90\% hydrogen peroxide (H2O2) as oxidizer. A variable area cavitating venturi as a dynamic flow controller was used to throttle the mass flow rate of H2O2. A catalytic bed was equipped to decompose H2O2 and ignite the fuel grain. Tube fuel grains of different port diameters and same length/diameter (L/D) ratio were tested. The minimum and maximum thrust achieved was 165.7 N and 1251 N, respectively. The maximum turn down and turn up ratio in tests were 5.32:1 and 2.1:1 respectively, with stable combustion across the entire range.",
author = "Sheng Zhao and Guobiao Cai and Hui Tian and Nanjia Yu and Peng Zeng",
note = "Publisher Copyright: {\textcopyright} 2015 American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015 ; Conference date: 27-07-2015 Through 29-07-2015",
year = "2015",
doi = "10.2514/6.2015-3831",
language = "英语",
isbn = "9781624103216",
series = "51st AIAA/SAE/ASEE Joint Propulsion Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "51st AIAA/SAE/ASEE Joint Propulsion Conference",
}