Effective Downsizing of a 15kW Class Satellite Bus

Effective Downsizing of a 15kW Class Satellite Bus

著者名:

掲載資料名:

A collection of the 21st AIAA International Communications Satellite Systems Conference and Exhibit technical papers, Yokohama, Japan, 15-19 April 2003

シリーズ名:

AIAA Paper : AIAA International Communications Satellite Systems Conference

シリーズ巻号:

2003

発行年:

2003

巻:

v. 1

通号:

2003-2308

ペーパー番号:

AIAA-2003-2308

開始ページ:

697

終了ページ:

704

総ページ数:

8

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISBN:

9781563475962 [1563475960]

言語:

英語

請求記号:

A07400/032200 (v.1)

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001571
シリーズID:	PA00000160
会議名:	AIAA International Communications Satellite Systems Conference and Exhibit
回次:	21st
会議開催地:	Yokohama, Japan
会議開催年:	2003.04.15-2003.04.19

類似資料:

1 テクニカルペーパー Multifunctional Structure Spacecraft Bus Technology Ozaki, T., Usami, R., Hahn, S. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Development of 2.0L Turbocharged DISI Engine for Downsizing Application. Han, D., Han, S-K., Han, B-H., Kim, W-T. Society of Automotive Engineers
2 テクニカルペーパー System Level Evaluation of Recently Developed Satellite Bus Technologies. Ozaki, T., Kabashima, S., Tkada, S., Ogushi, T., Tabata, M. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Testing of Environmental Satellite Bus-Instrument Interfaces Using Engineering Models Gagnier, D., Hayner, R., Roza, M., Nosek, T., Razzaghi, A., Hendershot, J. American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Power Beaming Technology Demonstration Satellite for Solarbird(R) Space Solar Power System Hahn, S., Ishii, H., Ozaki, T., Kiritani, K., Funyu, T., Okamoto, T. American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Drowsiness Detection Using Facial Expression. Hachisuka, S., Kimura, T., Ishida, K., Nakatani, H., Ozaki, N. Society of Automotive Engineers
4 テクニカルペーパー Experimetal Characterization of Thermal, Mechanical and Electrical Properties of Graphite/Cyanate Ester Composites of Varying Fiber Volume Fractions. Hahn, S.E., Takeya, H., Ozaki, T. Society of Manufacturing Engineers	10 テクニカルペーパー Parallel optimal design of satellite bus structures using particle swarm optimization Y. Yoon, J. Moon, E. Lee, S. Kim, J. Kim American Institute of Aeronautics and Astronautics
5 テクニカルペーパー 100-300kg Class Satellite Standard Bus System Design and Applications Fukuzawa, K., Abe, N., Nakamura, S., Suzuki, R., Kimura, S., Akioka, M. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー A 20 W Class S-Band SSPA for Japanese Engineering Test Satellite ？ Ishida,H., Kawakami,Y., Shigaki,M., Maeda,H., Sasaki,T., Ohba,T. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー 20mN Class Xenon Ion Engine Operation on Orbit T. Ozaki, Y. Kasai, T. Nakagawa, T. Itoh, K. Kajiwara, M. Ikeda American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Thermal Modeling and Testing of an Avionics Board for a Nano-Class Free-Flying Satellite S. Miller, E. Marotta American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12