Study on Electrodes Design for MPD Thruster Using Water Propellant.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2025, v. 68, n. 2, p. 108, doi. 10.2322/tjsass.68.108
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- Publication type:
- Article
Works by Akira KAKAMI
Results: 15
1
2
Performance Evaluation of Combustion-controllable 0.1-N-Class Solid Propellant Microthrusters Using Laser Heating.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2021, v. 64, n. 2, p. 65, doi. 10.2322/tjsass.64.65
- By:
- Publication type:
- Article
3
Characterization of a Liquid-propellant Pulsed Plasma ThrusterUsing Various Nozzle Configurations.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Science, 2019, v. 62, n. 4, p. 184, doi. 10.2322/tjsass.62.184
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- Publication type:
- Article
4
Performance of Gas-Generator-Type Hybrid Thruster Using a Laser Ignition.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 5, p. 802, doi. 10.2322/tastj.19.802
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- Publication type:
- Article
5
Application of a Pulsating Voltage Drive to an Anode-Layer-Type Hall Thruster.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 5, p. 621, doi. 10.2322/tastj.19.621
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- Publication type:
- Article
6
Performance of a Throttleable Solid Propellant Microthruster Using Laser Heating.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 598, doi. 10.2322/tastj.19.598
- By:
- Publication type:
- Article
7
Magneto Plasma Dynamic Thruster Using Water Propellant.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 523, doi. 10.2322/tastj.19.523
- By:
- Publication type:
- Article
8
N<sub>2</sub>O/DME Bipropellant Thruster with Premixer.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 3, p. 442, doi. 10.2322/tastj.19.442
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- Publication type:
- Article
9
A Horizontal-Pendulum Type Thrust Stand for Evaluating Higher Frequency Variation by Applying Acceleration Measurement to Null-Balance Method.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 2, p. 175, doi. 10.2322/tastj.17.175
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- Publication type:
- Article
10
400-V Bus-Direct Driven High-Power Arcjet Thruster Using Dimethyl Ether as Additive for Extending Lifetime.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 2, p. 155, doi. 10.2322/tastj.17.155
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- Publication type:
- Article
11
Effect of Carbon Black Diameter on Performance for a Throttleable Solid Propellant Microthruster Using Laser Heating.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2018, v. 16, n. 7, p. 668, doi. 10.2322/tastj.16.668
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- Publication type:
- Article
12
Influence of Injector for Performance of N<sub>2</sub>O/DME Bipropellant Thruster.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2018, v. 16, n. 2, p. 177, doi. 10.2322/tastj.16.177
- By:
- Publication type:
- Article
13
Performance Evaluation of a Throttleable Solid Propellant Thruster Using Laser Heating.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 61
- By:
- Publication type:
- Article
14
Improvement of Combustion Stability of N2O/DME Bipropellant in Vacuum.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 73
- By:
- Publication type:
- Article
15
Effect of Capacitance on the Performance of a Di-methyl Ether Pulsed Plasma Thruster.
- Published in:
- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 1
- By:
- Publication type:
- Article