Works matching IS 18840485 AND DT 2019 AND VI 17 AND IP 3
Results: 22
General Characteristics of Free-Return Ensured Orbit Insertion and Trajectory Design with MOI Robustness in MMX Mission.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 404, doi. 10.2322/tastj.17.404
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Orbit Design for the Martian Moons Exploration Mission.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 398, doi. 10.2322/tastj.17.398
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Education in Aerospace Engineering: A Report on the 2016 KOSEN Space Camp.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 392, doi. 10.2322/tastj.17.392
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The Low-Cost Rocket with Low Melting Temperature Thermoplastic Propellant.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 350, doi. 10.2322/tastj.17.350
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Development of Avalanche PhotoDiode (APD) Type Electron Measurement Unit for Space Use Focused on Satellite Charging.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 380, doi. 10.2322/tastj.17.380
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Optimal Attitude Control for Spacecraft Using Two Variable-Speed Control Moment Gyros.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 371, doi. 10.2322/tastj.17.371
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Minimum Time Orbit Raising of Geostationary Spacecraft by Optimizing Feedback Gain of Steering Law.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 363, doi. 10.2322/tastj.17.363
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Development of Mid Density Carbon Phenolic Ablators for Future Re-Entry Capsules.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 354, doi. 10.2322/tastj.17.354
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Fracture Investigation of Hollow Cylindrical Tether during Space Debris Impact.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 383, doi. 10.2322/tastj.17.383
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Concept Design of Seamless Location Based Emergency Warning System with GNSS-Based Signals.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 344, doi. 10.2322/tastj.17.344
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Investigation of the Long-Term Change of the TANSO-FTS Pointing Characteristics for a Future Agile Pointing Mechanism.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 339, doi. 10.2322/tastj.17.339
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- Article
Ablative Performance of High Density Carbon Phenolic after Cold Soak Exposure.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 333, doi. 10.2322/tastj.17.333
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Investigation into Star Tracker Algorithms using Smartphones with Application to High-Precision Pointing CubeSats.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 327, doi. 10.2322/tastj.17.327
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Validation of a Lattice Boltzmann Model for Transient Cryogenic Two-phase Flow.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 321, doi. 10.2322/tastj.17.321
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Space-based Observation of Lunar Impact Flashes.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 315, doi. 10.2322/tastj.17.315
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Improved Reference Orbits for the Repeat-Ground-Track Missions EnMAP and Tandem-L.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 308, doi. 10.2322/tastj.17.308
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Preliminary Numerical Simulation of Flow around Spaceplane for Airframe Engine Integration.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 301, doi. 10.2322/tastj.17.301
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Orbit Verification Results of the De-Orbit Mechanism Demonstration CubeSat FREEDOM.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 295, doi. 10.2322/tastj.17.295
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Development and Flight Results of Solid Propulsion System for Enhanced Epsilon Launch Vehicle.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 289, doi. 10.2322/tastj.17.289
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Active Interruption of Motor Combustion for Ammonium-Perchlorate Composite Propellant.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 282, doi. 10.2322/tastj.17.282
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Propellant Flow Analysis within Electric Propulsion Test Facility.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 276, doi. 10.2322/tastj.17.276
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Estimation of Interior Density Distribution for Small Bodies: The Case of Asteroid Itokawa.
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- Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 270, doi. 10.2322/tastj.17.270
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