Controlling Parameters for Fuel Regression Rate of Swirling-oxidizer-flow-type Hybrid Rocket Engine

48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ◽

10.2514/6.2012-4106 ◽

2012 ◽

Author(s):

Yuasa Saburo ◽

Shiraishi Noriko ◽

Hirata Kousuke

Keyword(s):

Rocket Engine ◽

Hybrid Rocket ◽

Regression Rate ◽

Flow Type ◽

Hybrid Rocket Engine

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Experimental Investigation of Fuel Regression Rate of Low-Melting-Point Thermoplastic Fuels in the Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES AEROSPACE TECHNOLOGY JAPAN ◽

10.2322/tastj.16.267 ◽

2018 ◽

Vol 16 (3) ◽

pp. 267-273

Author(s):

Yo KAWABATA ◽

Ayana BANNO ◽

Yutaka WADA ◽

Kohei OZAWA ◽

Toru SHIMADA ◽

...

Keyword(s):

Experimental Investigation ◽

Melting Point ◽

Rocket Engine ◽

Hybrid Rocket ◽

Regression Rate ◽

Flow Type ◽

Hybrid Rocket Engine

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Performance and Regression Rate Characteristics of 5-kN Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

Journal of Propulsion and Power ◽

10.2514/1.b36239 ◽

2017 ◽

Vol 33 (4) ◽

pp. 891-901 ◽

Author(s):

Takashi Sakurai ◽

Saburo Yuasa ◽

Hideyuki Ando ◽

Koki Kitagawa ◽

Toru Shimada

Keyword(s):

Rocket Engine ◽

Hybrid Rocket ◽

Regression Rate ◽

Flow Type ◽

Hybrid Rocket Engine

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DEVELOPMENT OF TEST FACILITIES FOR 5 KN-THRUST HYBRID ROCKET ENGINES AND A SWIRLING-OXIDIZER-FLOW-TYPE HYBRID ROCKET ENGINE FOR TECHNOLOGY DEMONSTRATION

International Journal of Energetic Materials and Chemical Propulsion ◽

10.1615/intjenergeticmaterialschemprop.2017011994 ◽

2016 ◽

Vol 15 (6) ◽

pp. 435-451 ◽

Author(s):

Koki Kitagawa ◽

Saburo Yuasa ◽

Takashi Sakurai ◽

S. Hatagaki ◽

N. Shiraishi ◽

...

Keyword(s):

Rocket Engine ◽

Rocket Engines ◽

Hybrid Rocket ◽

Flow Type ◽

Technology Demonstration ◽

Hybrid Rocket Engine

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Combustion Experiment to Evaluate a LOX Vaporization Nozzle for a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine with a 1500N-Thrust

SPACE TECHNOLOGY JAPAN THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ◽

10.2322/stj.6.47 ◽

2007 ◽

Vol 6 ◽

pp. 47-54 ◽

Author(s):

Koki KITAGAWA ◽

Toshiaki SAKURAZAWA ◽

Saburo YUASA

Keyword(s):

Rocket Engine ◽

Hybrid Rocket ◽

Flow Type ◽

Combustion Experiment ◽

Hybrid Rocket Engine

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Static Burning Tests on a Bread Board Model of Altering-intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

52nd AIAA/SAE/ASEE Joint Propulsion Conference ◽

10.2514/6.2016-4964 ◽

2016 ◽

Author(s):

Kohei Ozawa ◽

Tomoaki Usuki ◽

Genki Mishima ◽

Koki Kitagawa ◽

Masato Yamashita ◽

...

Keyword(s):

Rocket Engine ◽

Hybrid Rocket ◽

Flow Type ◽

Hybrid Rocket Engine

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Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine

10.2514/6.1998-3348 ◽

1998 ◽

Author(s):

William Knuth ◽

Martin Chiaverini ◽

Daniel Gramer ◽

J. Sauer

Keyword(s):

Experimental Investigation ◽

Rocket Engine ◽

Hybrid Rocket ◽

Regression Rate ◽

Hybrid Rocket Engine

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Prediction of Time Variation of Ballistic Parameters For a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine using Burning Data

46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ◽

10.2514/6.2010-6874 ◽

2010 ◽

Author(s):

Noriko Shiraishi ◽

Saburo Yuasa

Keyword(s):

Time Variation ◽

Rocket Engine ◽

Hybrid Rocket ◽

Flow Type ◽

Hybrid Rocket Engine

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Prediction of Time Variation of Ballistic Parameters for a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ◽

10.2322/jjsass.61.31 ◽

2013 ◽

Vol 61 (2) ◽

pp. 31-37

Author(s):

Noriko SHIRAISHI ◽

Saburo YUASA

Keyword(s):

Time Variation ◽

Rocket Engine ◽

Hybrid Rocket ◽

Flow Type ◽

Hybrid Rocket Engine

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Unsteady Numerical Simulation on Axial and Tangential Oxidizer Injection in Altering-intensity Swirling Oxidizer Flow Type Hybrid Rocket Engine

The Proceedings of Conference of Kyushu Branch ◽

10.1299/jsmekyushu.2018.71.b43 ◽

2018 ◽

Vol 2018.71 (0) ◽

pp. B43

Author(s):

Shota GOTO ◽

Kohei OZAWA ◽

Tomoki UZAKI ◽

Yoshiki NISHIKAWA ◽

Nobuyuki TSUBOI

Keyword(s):

Numerical Simulation ◽

Rocket Engine ◽

Hybrid Rocket ◽

Flow Type ◽

Hybrid Rocket Engine ◽

Unsteady Numerical Simulation

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Pre-design study of a sub-orbital vehicle concept and study of the N2O/Paraffin regression rate in a scaled hybrid rocket engine

18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2012-5875 ◽

2012 ◽

Author(s):

K. Boughaba ◽

P. Hendrick ◽

A. Mahajan ◽

M. Lefebvre ◽

C. Van de Velde ◽

...

Keyword(s):

Rocket Engine ◽

Vehicle Concept ◽

Hybrid Rocket ◽

Design Study ◽

Regression Rate ◽

Hybrid Rocket Engine ◽

Orbital Vehicle

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