Immunoglobulin resistance in Kawasaki disease with chronic granulomatous disease.
- Published in:
- Pediatrics International, 2012, v. 54, n. 3, p. e32, doi. 10.1111/j.1442-200X.2011.03523.x
- By:
- Publication type:
- Article
Works matching AU Yasuyuki YANO
Results: 12
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
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
- By:
- Publication type:
- Article
4
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
5
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
6
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
- By:
- Publication type:
- Article
7
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
- By:
- Publication type:
- Article
8
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
- By:
- Publication type:
- Article
9
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
- By:
- Publication type:
- Article
10
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
11
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
12
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