On the Structures of the Low Altitude Stationary Flight Test Vehicle-Reference-Cited by-同舟云学术

On the Structures of the Low Altitude Stationary Flight Test Vehicle

Published:2005-09-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences
language:
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Author:

Maekawa Shoji,Takegaki Atushi

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-7407

Reference9 articles.

1. 1Nakadate, M. "Flight Test Overview of Low Altitude Stationary Flight Test Vehicle", The Fifth Stratospheric PlatformSystems Workshop, Feb.23-24,2005,Tokyo,Japan.

2. 2Kohno, T. "Flight Control of Low Altitude Stationary Flight Test Vehicle", The Fifth Stratospheric Platform Systems Workshop, Feb.23-24,2005, Tokyo, Japan.

3. 3Harada, K. "Buoyancy Control of Ground to Stratosphere/Low Altitude Stationary Flight Test Vehicles", The Fifth Stratospheric PlatformSystems Workshop, Feb.23-24, 2005, Tokyo, Japan.

4. 4Sasa, S., Yoshida, H., Ohashi, K., Miyazaki, T. "Flight Test Overview of Ground to Stratosphere Flight Test Vehicle",The FifthStratospheric PlatformSystems Workshop, Feb.23-24,2005, Tokyo, Japan.

5. 5Sasaki, Y., Eguchi, K., Kohno, T., Maekawa, S. "Scenario for Development of the SPF Airship Technology Demonstrator",The FifthStratospheric PlatformSystems Workshop, Feb.23-24,2005, Tokyo, Japan.

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