@inproceedings{5ec62fa00ce74d39a201cbbc212d8ccf,
title = "Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane",
abstract = "Hybrid rocket engine with multi-section swirl injection method was designed and tested for the flight experiments of subscale space plane. Combustion experiments were carried out with high density polyethylene (HDPE) and paraffin fuel and gaseous oxygen with several combustion conditions. Fundamental data for flyable hybrid rocket including usefulness of high pressure CFRP oxygen tank have been revealed. Flight simulation using the measured thrust data clarified the reachable altitude and required thrust to future flight experiments.",
author = "Kengo Ohe and Masato Mizuchi and Shigeru Aso and Yasuhiro Tani and Sho Ohyama and Kentaro Araki and Hiroshi Tada and Toru Shimada",
year = "2014",
month = jan,
day = "1",
doi = "10.2514/6.2014-3954",
language = "English",
series = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014",
note = "50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 ; Conference date: 28-07-2014 Through 30-07-2014",
}