Applicability of CFRP materials to the cryogenic propellant tank for reusable launch vehicle (RLV)

Y. Morino; T. Shimoda; T. Morimoto; T. Ishikawa; T. Aoki

doi:10.1163/156855101753415364

Applicability of CFRP materials to the cryogenic propellant tank for reusable launch vehicle (RLV)

Y. Morino^*, T. Shimoda, T. Morimoto, T. Ishikawa, T. Aoki

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

20 Citations (Scopus)

Abstract

It is essential to utilize carbon fiber reinforced plastics (CFRP) for main structural materials of cryogenic propellant tanks in order to realize the drastic weight reduction needed for efficient reusable space transportation systems. Recently developed toughened CFRP materials. which are expected to show good cryogenic properties, are considered promising candidates for these kinds of applications. The present study investigates cryogenic properties of candidate materials and structural elements, including Y-joint structural models. 300 mm diameter filament wound tank and 600 mm diameter lay up tanks were fabricated and tested. Based on these experimental data, the feasibility of a CFRP cryogenic tank is discussed and future research tasks are proposed. This research is being conducted under the cooperation contract between NASDA and NAL.

Original language	English
Pages (from-to)	339-347
Number of pages	9
Journal	Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials
Volume	10
Issue number	4
DOIs	https://doi.org/10.1163/156855101753415364
Publication status	Published - 2001
Externally published	Yes

Keywords

Composites
Cryogenic tank
RLV

ASJC Scopus subject areas

Ceramics and Composites

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10.1163/156855101753415364

Cite this

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abstract = "It is essential to utilize carbon fiber reinforced plastics (CFRP) for main structural materials of cryogenic propellant tanks in order to realize the drastic weight reduction needed for efficient reusable space transportation systems. Recently developed toughened CFRP materials. which are expected to show good cryogenic properties, are considered promising candidates for these kinds of applications. The present study investigates cryogenic properties of candidate materials and structural elements, including Y-joint structural models. 300 mm diameter filament wound tank and 600 mm diameter lay up tanks were fabricated and tested. Based on these experimental data, the feasibility of a CFRP cryogenic tank is discussed and future research tasks are proposed. This research is being conducted under the cooperation contract between NASDA and NAL.",

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AU - Morino, Y.

AU - Shimoda, T.

AU - Morimoto, T.

AU - Ishikawa, T.

AU - Aoki, T.

PY - 2001

Y1 - 2001

N2 - It is essential to utilize carbon fiber reinforced plastics (CFRP) for main structural materials of cryogenic propellant tanks in order to realize the drastic weight reduction needed for efficient reusable space transportation systems. Recently developed toughened CFRP materials. which are expected to show good cryogenic properties, are considered promising candidates for these kinds of applications. The present study investigates cryogenic properties of candidate materials and structural elements, including Y-joint structural models. 300 mm diameter filament wound tank and 600 mm diameter lay up tanks were fabricated and tested. Based on these experimental data, the feasibility of a CFRP cryogenic tank is discussed and future research tasks are proposed. This research is being conducted under the cooperation contract between NASDA and NAL.

AB - It is essential to utilize carbon fiber reinforced plastics (CFRP) for main structural materials of cryogenic propellant tanks in order to realize the drastic weight reduction needed for efficient reusable space transportation systems. Recently developed toughened CFRP materials. which are expected to show good cryogenic properties, are considered promising candidates for these kinds of applications. The present study investigates cryogenic properties of candidate materials and structural elements, including Y-joint structural models. 300 mm diameter filament wound tank and 600 mm diameter lay up tanks were fabricated and tested. Based on these experimental data, the feasibility of a CFRP cryogenic tank is discussed and future research tasks are proposed. This research is being conducted under the cooperation contract between NASDA and NAL.

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Applicability of CFRP materials to the cryogenic propellant tank for reusable launch vehicle (RLV)

Abstract

Keywords

ASJC Scopus subject areas

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