Design and testing of the HOPE-X HSFD-II landing system-Reference-Cited by-同舟云学术

Design and testing of the HOPE-X HSFD-II landing system

Published:2001-05-21 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar
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Author:

Gardinier Debra¹,Yanagihara M.²,Kobayashi T.³,Amito Atsushi⁴

Affiliation:

1. Irvin Aerospace, Inc., Santa Ana, CA

2. National Aerospace Lab., Tokyo, Japan

3. National Space Development Agency of Japan, Tokyo

4. Fuji Heavy Industries, Ltd., Tochigi, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

Reference6 articles.

1. IrvinAerospace,Inc.,High SpeedFlight Demonstrator(HSFD-II)AirbagImpact Attenuation (ABIAS)PreliminaryDesign Report,GIR85-927,Rev.A.,March 31,2000.

2. IrvinAerospace,Inc.,High SpeedFlight Demonstrator(HSFD-II)ParachuteSubsystem PreliminaryDesignReport,GIR85-920,Rev. A.,March 31,2000.

3. IrvinAerospace,Inc.,High SpeedFlight Demonstrator(HSFD-II)FlightTermination SubsystemPreliminaryDesignReport,GIR85-947,Rev.A.,March 31, 2000.

4. IrvinAerospace,Inc.,High SpeedFlight Demonstrator (HSFD-II)ParachuteSubsystem CriticalDesignReport,GIR85-921,Rev.A., September 27,2000.

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