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Volumn 66, Issue 1, 2006, Pages 55-70

Study of cryogenic mechanical strength and fracture behavior of adhesives for CFRP tanks of reusable launch vehicles

Author keywords

Adhesive; CFRP composite; Cryogenic; FEM; Filament winding; Propellant tank; Shear Strength; Tensile Strength

Indexed keywords

ADHESIVE THICKNESS; BONDING STRENGTHS; CFRP COMPOSITES; PROPELLANT TANKS;

EID: 33645136223     PISSN: 1880148X     EISSN: 1880148X     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (8)

References (11)
  • 1
    • 0025792786 scopus 로고
    • Adhesive bonding peek/IM-6 composite for cryogenic applications
    • April
    • Goeders and Perry J.L., "Adhesive Bonding Peek/IM-6 Composite for Cryogenic Applications," 36th International SAMPE Symposium, Vol.36, pp.348-361, April 1991.
    • (1991) 36th International SAMPE Symposium , vol.36 , pp. 348-361
    • Goeders1    Perry, J.L.2
  • 2
    • 3142783379 scopus 로고    scopus 로고
    • Bonding and sealing evaluation for cryogenic tanks
    • Contract NAS1-96014, August
    • Glass, D. E., "Bonding and Sealing Evaluation for Cryogenic Tanks," NASA Contractor Report 201734, Contract NAS1-96014, August 1997.
    • (1997) NASA Contractor Report 201734
    • Glass, D.E.1
  • 3
    • 33645164645 scopus 로고    scopus 로고
    • Work Performed for McDonnell Douglas Space Systems, Co. by Materials Research & Engineering, Inc., PO No. 96674005H, February 29
    • Anon., "Double Lap Shear and T-Peel Tests in a Temperature Range from -423oF to 350oF," Work Performed for McDonnell Douglas Space Systems, Co. by Materials Research & Engineering, Inc., PO No. 96674005H, February 29, 1996.
    • (1996) Double Lap Shear and T-Peel Tests in A Temperature Range from -423oF to 350oF
  • 4
    • 4444306591 scopus 로고    scopus 로고
    • Cryogenic test of CFRP scale tank for the future rocket plane propellant
    • Tokyo, November
    • Morimoto, T., Shimoda, T., and Morino, Y., "Cryogenic Test of CFRP Scale Tank for the Future Rocket Plane Propellant," Proceedings of the 37th Aircraft Symposium, pp. 541-544, Tokyo, November 1999.
    • (1999) Proceedings of the 37th Aircraft Symposium , pp. 541-544
    • Morimoto, T.1    Shimoda, T.2    Morino, Y.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.