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The Institute of Space and Astronautical Science Report SP |
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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 Vapor-State 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 Gravity-Assisted Heat Pipe. | ||
Y. Ikeda and S Onuma |
Heat Transfer of Mesh-Wick Heat-Pipes (Bottom Heat Mode). |
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T. Matsuoka, K. Negishi, K. Kaneko, M. Hirashima, Y. Nishikawa and M. Taguchi | An Arranging Method on L/D of Two-Phase Closed Thermosyphons. | ||
M. Murakami, K. Arai and Y. Kojima | A Statistical Treatment of Accerelated Life Test Data for Copper-Water Heat Pipes. | ||
Y. Miyazaki, Y. Kuriyama and M. Furukawa | Forced-Convective 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 Gas-Steam 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 Three-Dimensional 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 | Laser-Assisted 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.6-8 | No.9-10 | No.11-12 | No.13 | No.14 | No.15-17 | |
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