Yukio Shimizu

发表

Measurement of Velocity and Power Balance in a Two-Dimensional MPD Arcjet

Ikkoh Funaki, Kyoichiro Toki, Kiyoshi Kinefuchi, 2005 .

MPD arcjet system performance test

Shinji Morimoto, Yukio Shimizu, K. Kuriki, 1985 .

1000 Robots, Spaceships, and Other Tin Toys

Yukio Shimizu, Terhisa Kitahara, 2003 .

The MPD arcjet thruster system for Electric Propulsion Experiment onboard Space Flyer Unit

Hiroshi Suzuki, Kyoichiro Toki, Kyoichi Kuriki, 1990 .

Feasibility Study on Performance Enhancement Options for the ECR Ion Thruster µ10

Satoshi Hosoda, Hitoshi Kuninaka, Hiroshi Hayashi, 2008 .

Triplex digital flight control system for the STOL research aircraft'Aska'

Akira Watanabe, Tadao Uchida, Noriaki Okada, 1988 .

Accomplishment and prospect of isas electric propulsion

Hitoshi Kuninaka, Kyoichiro Toki, Kyoichi Kuriki, 2002 .

Experimental Verification of the Nozzle Shape Optimization for Self-Field MPD Thruster

Hitoshi Kuninaka, Ikkoh Funaki, Kyoichiro Toki, 2005 .

Electric Propulsion Experiment (EPEX) onboard Space Flyer Unit (SFU)

Hiroshi Suzuki, Kyoichiro Toki, Kyoichi Kuriki, 1992 .

Construction of mountain airport by high embankment.

Toshio Aida, Yukio Shimizu, Ichiro Kono, 1989 .

Design of a multiprocessor based satellite packet communication processor for integrated services networks

Hiroaki Kojima, Tomonori Takizuka, Kazuhito Matsuo, 1983 .

Yukio Shimizu, 1989 .

Electric Propulsion Experiment onboard Space Flyer Unit

Yukio Shimizu, K. Toki, K. Kuriki, 1990 .

A Study of X-Field Head

Yukio Shimizu, Yasuhiko Izumi, Satoshi Takeguchi, 1968 .

DEVELOPMENT OF MICROWAVE DISCHARGE ION ENGINE SYSTEM FOR ASTEROID SAMPLE AND RETURN MISSION MUSES-C

Hitoshi Kuninaka, Shin Satori, Ikkoh Funaki, 1997 .

Research and Development of Magnetoplasmadynamic Arcjets for Future High-Power Space Applications

Kyoichiro Toki, Yukio Shimizu, 1999 .

An Ion Machined Accelerator Grid for the ECR Ion Thruster µ20

Satoshi Hosoda, Hitoshi Kuninaka, Kazutaka Nishiyama, 2008 .

Vertical axis wind turbine designed aerodynamically at Tokai University

Yasushi Kato, Yukio Shimizu, Kazuya Seki, 1981 .

Study of Low-Power MPD Propulsion for Future High-Power Trend

Kyoichiro Toki, Yukio Shimizu, Y. Shimizu, 2002 .

Development of an Ion Engine System for MUSESC Asteroid Exploration Mission

Hitoshi Kuninaka, Kyoichiro Toki, Kazutaka Nishiyama, 2002 .

Result of 18,000-hour endurance test on microwave discharge ion thruster engineering model

Hitoshi Kuninaka, Kyoichiro Toki, Kazutaka Nishiyama, 2000 .

Development of an Endurance Test Facility for Microwave Discharge Ion Engine System.

Hitoshi Kuninaka, Ikkoh Funaki, Shin Satori, 1999 .

Experimental Demonstration of Microwave Discharge Ion Engine with 10,000 sec Isp

Satoshi Hosoda, Hiroyuki Koizumi, Hitoshi Kuninaka, 2009 .

Total Electrode Fall Measurement in a Parallel-Plate Magnetoplasmadynamic Thruster

Hitoshi Kuninaka, Ikkoh Funaki, Kyoichiro Toki, 2009 .

Thermal analysis and thrust performance of a low power arcjet thruster

Yukio Shimizu, K. Kuriki, K. Toki, 1990 .

Ground Chamber Measurements of the Electromagnetic Emissions from the Hayabusa Ion Engine

Hitoshi Kuninaka, Ikkoh Funaki, Kyoichiro Toki, 2007 .

Experimental Measurement of Total Sheath Fall Voltage in an MPD Thruster

Hitoshi Kuninaka, Ikkoh Funaki, Kyoichiro Toki, 2008 .

Fundamental Research of High Specific Impulse Microwave Discharge Ion Engine

Hitoshi Kuninaka, Yoshinori Nakayama, Hiroshi Hayashi, 2007 .

Hayabusa's Way Back to Earth by Microwave Discharge Ion Engines

Satoshi Hosoda, Junichiro Kawaguchi, Hiroyuki Koizumi, 2010 .

R&D on 10,000 sec Isp Ion Engine driven by Microwave

Satoshi Hosoda, Hiroyuki Koizumi, Hitoshi Kuninaka, 2008 .

Genetic-algorithm-based method to optimize spatial profile utilizing characteristics of electrostatic actuator deformable mirror

Sakae Kawato, Takao Kobayashi, Yukio Shimizu, 2008 .

Flight Report during Two Years on HAYABUSA Explorer Propelled by Microwave Discharge Ion Engines

Hitoshi Kuninaka, Tetsuya Yamada, Kazutaka Nishiyama, 2005 .

On-Orbit Demonstration of a Pulsed Self-Field Magnetoplasmadynamic Thruster System

Yukio Shimizu, K. Kuriki, K. Toki, 2000 .

Flight Status of Cathode-Less Microwave Discharge Ion Engines Onboard HAYABUSA Asteroid Explorer

Hitoshi Kuninaka, Kyoichiro Toki, Kazutaka Nishiyama, 2004 .

Status of Microwave Discharge Ion Engines on Hayabusa Spacecraft

Satoshi Hosoda, Hiroyuki Koizumi, Hitoshi Kuninaka, 2007 .

Idealized model for plasma acceleration in an MHD channel

Yukio Shimizu, K. Kuriki, Y. Shimizu, 1983 .

Laboratory Experiment of Plasma Flow Around Magnetic Sail

Hiroshi Yamakawa, Ikkoh Funaki, Yoshinori Nakayama, 2007 .

Verification Tests of Carbon-Carbon Composite Grids for Microwave Discharge Ion Thruster

Hitoshi Kuninaka, Kyoichiro Toki, Kazutaka Nishiyama, 2002 .

Thrust Performance of a Regeneratively Cooled Low-Power Arcjet Thruster

Tetsuya Yamada, Kyoichiro Toki, Kyoichi Kuriki, 1992 .

Endurance Test of Microwave Discharge Ion Thruster System for Asteroid Sample Return Midon MUSES-C

Hitoshi Kuninaka, Shin Satori, Kyoichiro Toki, 1998 .

Application of MPD thruster systems to interplanetary missions

Yukio Shimizu, K. Kuriki, K. Toki, 1986 .

Powered Flight of HAYABUSA in Deep Space

Junichiro Kawaguchi, Hitoshi Kuninaka, Tetsuya Yamada, 2006 .

Current distribution in a quasi-steady MPD arcjet

Yukio Shimizu, K. Kuriki, Y. Kunii, 1982 .