Works matching IS 18840485 AND DT 2021 AND VI 19 AND IP 4
Results: 23
Trial of a New Educational Use of a Nanosatellite: Workshop Planning Observations Using the Stars-AO Satellite for High School and Junior High School Students.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 616, doi. 10.2322/tastj.19.616
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Development Status of 4N Class Low-cost Thrusters Manufactured by 3D-Printed Metals.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 612, doi. 10.2322/tastj.19.612
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Shape of a Square Solar Sail Consisted of Four Trapezoid Petals with Curved Thin-Film Devices: Simulations and Experiments.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 604, doi. 10.2322/tastj.19.604
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Performance of a Throttleable Solid Propellant Microthruster Using Laser Heating.
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- 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
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Unsteady Testing of an Ablation Sensor in Torch Flame.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 591, doi. 10.2322/tastj.19.591
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Optimization for Solar Angle Free Attitude Motion Model by Solar Sail IKAROS.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 584, doi. 10.2322/tastj.19.584
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Flow Analysis around Spaceplane for Airframe Engine Integration by CFD.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 577, doi. 10.2322/tastj.19.577
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Study on Hysteresis of Combustion Oscillation in Continuously Variable Resonance Combustor using Deep Neural Network.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 570, doi. 10.2322/tastj.19.570
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Orbit Maintenance for Quasi-Periodic Orbit in Earth-Moon System.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 562, doi. 10.2322/tastj.19.562
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Design and Guidance for Robust Orbit Raising Trajectory of All-Electric Propulsion Geostationary Satellites.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 553, doi. 10.2322/tastj.19.553
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Sparse Optimal Control for Nonlinear Trajectory Design in Three-Body Problem.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 545, doi. 10.2322/tastj.19.545
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Numerical Prediction of the Spontaneous Ignition of Cool Flame for the Microgravity Experiment by Using Sounding Rocket.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 539, doi. 10.2322/tastj.19.539
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Automatic Landing System with Consideration of Constraints Using Dynamic Window Approach.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 529, doi. 10.2322/tastj.19.529
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Magneto Plasma Dynamic Thruster Using Water Propellant.
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- 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
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Return and Recovery Operation of the Hayabusa2 Sample Return Capsule.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 514, doi. 10.2322/tastj.19.514
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- Article
Improving Performance of WAX-Based Hybrid Rocket Solid Fuel with Adding Ammonium Nitrate.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 507, doi. 10.2322/tastj.19.507
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- Article
Propellantless Close-Range Guidance for Small Satellite Docking Using Simple Electromagnetic Devices.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 500, doi. 10.2322/tastj.19.500
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Automated Image Processing Module for Images Captured by Earth Observation Microsatellite Diwata-1 as Support for Ground Station Operations.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 493, doi. 10.2322/tastj.19.493
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On-Board Computers for Micro-Satellites.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 485, doi. 10.2322/tastj.19.485
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A Feasible Study of In-Situ Measurements of Light Isotopes and Organic Molecules with High Resolution Mass Spectrometer MULTUM on the OKEANOS Mission.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 477, doi. 10.2322/tastj.19.477
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Study of a Planetary Exploration Rover with a Hinge-type Center-of-gravity Shift Mechanism.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 469, doi. 10.2322/tastj.19.469
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Stability Analysis of Spacecraft Motion in the Vicinity of a Second Body in the Elliptic Restricted Three-body Problem.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 461, doi. 10.2322/tastj.19.461
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Separation Experiment for OMOTENASHI Moon Lander at Extremely High Spin Rates.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 4, p. 453, doi. 10.2322/tastj.19.453
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