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機構	日期	題名	作者
淡江大學	1999-10	The Passive Magnetic Stabilization used Magnetic Rods for a Microsatellite TUU SAT-1	Lin, C. H.; Hong, Z. C.; Shih, C. H.; Chuang, C. K.
淡江大學	1999-01	The Desigh and Fabrication of TUU SAT-1 Ground Station by Students	Zhen, C. E.; Hong, Z. C.; Lin, C. H.; Lee, C. C.
淡江大學	1997-12	Analysis of the Unsteady State Temperature Distribution of Microsatellite Under Stabilization Effects	Lee, S. R.; Wu, Kuang; Hong, Z. C.; Peng, K. T.
淡江大學	1997-12	Comparison of Magnetic and Aerodynamics Stabilization for a Microsatellite	Hong, Z. C.; Hu, W. H.; Chen, Y. H.; Chern, J. S.
淡江大學	1997-01	Aerodynamic and Stabilization Gravity Gradient Stabilization for Micro-Satellite	Chen, Y. H.; Hong, Z. C.; Chern, J. S.
淡江大學	1996-09	Analysis and design for the passive thermal control temperature distribution of a square and a hexagon pillar micro-satellite	Lee, S. R.; Hsiau, S. S.; Hong, Z. C.; Lue, L. S.
淡江大學	1996-07	Flight Envelopes for Hypersonic Aerorendezvous at Constant Altitude	Chen, Y. H.; Chen, S. J.; Chern, J. S.; Hong, Z. C.
淡江大學	1996-07	Effect Thrust Angle Constraint on the Payload Ratio of a Laser Propulsion System	Hong, Z. C.; Hsu, F. C.
淡江大學	1995-10	Optimal Turning Winged Space Vehicles st Constant Altitude	Chern, J. S.; Chen, Y. H.; Hong, Z. C.
淡江大學	1995-10	Overall Payload Ratio of A Combined Laser and Chemical Propulsion System for GEO Launch	Hong, Z. C.; Liu, J. M.; Chern, J. S.
淡江大學	1995-10	Shock-Induced Mixing Enhancement of Supersonic Turbulent Reacting Ramjet Flows	Hong, Z. C.; Shih, M. S.; Hwang, K. W.
淡江大學	1995-08	Effect of Laser Power Limitation on Single-Stage to GEO Launch	Hong, Z. C.; Chern, J. S.; Liu, J. M.
淡江大學	1995-01	A PDF Description of Turbulent Plane Couette Flow	Hong, Z. C.; Lin, C.; Chen, M. H.
淡江大學	1995-01	Laser Propulsion System Performance Requirements for Single Stage to GEO Launch	Hong, Z. C.; Chern, C. Y.; Chern, J. S.
淡江大學	1994-10	Aero Rendezvous Optimization and Limitation of Winged Space Vehicles	Chern, J. S.; Hong, Z. C.; Chen, Y. H.; Liu, J. M.
淡江大學	1994-10	Laser Propulsion System Performance Requirements for Single Stage to GEO Launch	Hong, Z. C.; Chern, C. Y.; Chern, J. S.
淡江大學	1994-08	Flight Envelope for Aero-Rendezvous with small Initial Heading	Chern, J. S.; Hong, Z. C.; Chern, Y. H.
淡江大學	1994-08	Flight Envelopes for Hypersonic Aero-Rendezvous with Large Initial Heading	Hong, Z. C.; Chen, S. J.; Chern, J. S.
淡江大學	1994-02	Direct Ascent to GEO with Dynamic Pressure and Thrust Acceleration Constraints	Hong, Z. C.; Chern, J. S.; Chang, C. Y.
淡江大學	1994-02	Optimal Turning for Aero-Rendezvous with G and Heating Rate Constraints	Chern, J. S.; Hong, Z. C.; Chern, Y. S.; Chern, S. J.
淡江大學	1993-10	Approximate Chattering ARC for Minimun Time Flight	Chern, J. S.; Hong, Z. C.
淡江大學	1993-10	Effect of Fuel-Inlet Location on Combustor Characteristics within Scramjet Dump Combustor	Hong, Z. C.; Hwang, K. W.
淡江大學	1993-07	Modelling Analysis of a Simulated Afterburner with Twin V-gutter Flameholders and Swirling Inlet.	Hong, Z. C.; Lin, C. K.; Huang, J. J.; Chen, M. H.
淡江大學	1993-01	PDF Description of Turbulent Couette Flow	Hong, Z. C.; Lin, C.; Chen, M. H.
淡江大學	1992-05	Numerical Simulation of Transonic Seperated Flow over A Hemisphere Cylinder at Moderate Angle of Attack	Wu, A. M.; Hong, Z. C.; Wang, C. S.

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