Cryogenic mechanical properties of CF/polymer composites for tanks of reusable rockets

• AOKI T.

  Department of Aeronautics and Astronautics, University of Tokyo

• ISHIKAWA T.

  National Aerospace Laboratory

• KUMAZAWA H.

  National Aerospace Laboratory

• MORINO Y.

  National Space Development Agency of Japan

収録刊行物

• Advanced composite materials : the official journal of the Japan Society for Composite Materials

  Advanced composite materials : the official journal of the Japan Society for Composite Materials 10 (4), 349-356, 2001-12-01

キーワード

• Mechanical properties
• cryogenics
• propellant tank
• matrix crack
• delamination
• interlaminar fracture toughness

詳細情報

• CRID: 1572261549595462656
• NII論文ID: 10008225770
• NII書誌ID: AA10744021
• ISSN: 09243046
• 本文言語コード: en
• データソース種別:
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