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The Institute of Space and Astronautical Science Report SP 

No. 
Year 
Author 
Title 
6  1988.3  Proceedings of the Symposium on Mechanics for Space Flight.  
K. Oshima  Preface  
H.L. Chen and K. Oshima  Numerical Analysis of Reconnection of Vortex Rings.  
A. Yamashita and Y. Oshima  Vortex Filament Simulation for the Crosslinking Vortex Rings.  
Y. Oshima and N. Izutsu  Crosslinking of Two Vortex Rings Side by Side.  
Y. Ishii and H. Kanda  Turbulence Transition in a Circular Pipe.  
H. Shirai  Absorption Characteristics of Si3N4 Ablation Layer Plasma.  
K. Etori  Thermostatistical Estimation of VaporState Molecules affected by Gravity in a Heat Pipe.  
F. Kaminaga, N. Tsuyuzaki, T. Saito, M. Konno and Y. Okamoto  An Experimental Investigation of Transient Characteristics in a GravityAssisted Heat Pipe.  
Y. Ikeda and S Onuma 
Heat Transfer of MeshWick HeatPipes (Bottom Heat Mode). 

T. Matsuoka, K. Negishi, K. Kaneko, M. Hirashima, Y. Nishikawa and M. Taguchi  An Arranging Method on L/D of TwoPhase Closed Thermosyphons.  
M. Murakami, K. Arai and Y. Kojima  A Statistical Treatment of Accerelated Life Test Data for CopperWater Heat Pipes.  
Y. Miyazaki, Y. Kuriyama and M. Furukawa  ForcedConvective Boiling in Small Diameter Tube.  
M. Hirashima, U. Nishikawa, M. Taguchi, K. Negishi, K. Kaneko and T. Matsuoka  Characteristics of Long Size Thermosyphons Made of Corrugated Tube.  
L.Z. Guang and K. Oshima  An Analysis of GasSteam Total Power Recovery Energy System.  
M. Inoue, K.Tsuchiya, A. Nakajima and C. Murakami  Nutational Stability of a Satellite Equipped with an Active Magnetic Momeutum Wheel.  
M. Hinada, I. Nakatani, K. Ninomiya, N. Muranaka, T. Namera, M. Uo and N. Ogura  Dynamics of Satellite with Radial Wire Antennas.  
7  1988.11  An Aerodynamics in Relation to an Aeroassisted Orbit Transfer Vehicle.  
T. Abe  Preface  
T. Abe  A Self consistent Tension Shell Structure for Application to Aerobraking Vehicle and its Aerodynamic Characteristics.  
H. Honma, A. Tsukamoto, T. Ohno and T. Tanaka  Generation and Observation of Strong Shock Waves in the Flight Regiemes of AOTV.  
K. Nanbu, S. Igarashi and Y. Watanabe  Hypersonic Rarefied Flows Around a Circular Disk Perpendicular to the Stream.  
K. V. Reddy, T. Fujiwara, T. Ogawa and K. Arashi  Computation of ThreeDimensional Chemically Reacting Viscous Flow around Rocket Body.  
S. Tanaka, K. Teshima, K. Ueno and M. Nishida  Flow Visualization of Sonic Jets Exhausting Counter to a Supersonic Free Stream Using Laser Induced Fluorescence Method.  
8  1988.12  Utilization of Laser Technology in Space.  
T. Abe  Preface  
T. Abe and T. Shimada  LaserAssisted Propulsion System Experiment on Space Flyer Unit.  
K. Maeno, H. Aoyama, A. Sakashita and Y. Hanaoka  Investigations of Advanced CO2 Supersonic Mixing Laser and Propulsion by Laser Absorption.  
C. Yamabe, K. Nakamura, H. Homma, M. Yamauchi, T. Okamoto, H. Ishihara, T. Nakamura, S. Takagi and K. Horii  Power Transmission by Using Laser Beams. 
 No.1  No.2  No.3  No.4  No.5  No.68  No.910  No.1112  No.13  No.14  No.1517  
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