Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Hirata Kohsuke"'
Autor:
Sakurai Takashi, Hirata Kohsuke, Shiraishi Noriko, Sezaki Chinatsu, Sakamoto Masafumi, Yuasa Saburo
Publikováno v:
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
The axial-direction fuel regression rates of the swirling-oxidizer-flow-type hybrid rocket engine were mesurred using PP fuel grains under the experimental conditions; grain length of 600 mm, intermediate oxygen mass flux Goitm up to about 120 kg/(m