Cryogenic composite tank design for next generation launch technology

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Abumeri, Galib H ^a   Kosareo, Daniel N ^b   Roche, Joseph M ^c  

^a QSS GROUP INC   (United States)

^b ZIN Technologies Inc   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE MECHANICS; COMPOSITE TANK; CRYOGENIC COMPOSITE TANKS; DAMAGE INITIATION; DAMAGE PROGRESSION; DESIGN CONCEPT; DESIGN PRESSURE; FINITE ELEMENT; INTERNAL PRESSURE; LIQUID HYDROGEN TANKS; LOW CYCLE FATIGUES; NEXT GENERATION LAUNCH TECHNOLOGIES; STRUCTURAL PERFORMANCE; TANK DESIGN;

DAMAGE DETECTION; DESIGN; FATIGUE DAMAGE; HYDROGEN; LIQUEFIED GASES; PRESSURIZATION; PROPULSION; STRUCTURAL ANALYSIS; TANKS (CONTAINERS);

DAMAGE TOLERANCE;

EID: 77957834855     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. s "Composite Tank Permeation and Crack Density Prediction and Verification", ASME Symposium on Space Applications of Composites, Washington, DC, 2003.
2. Greenberg, H.S., "Milestone 10-Test Report of Composite Tank Material Screening Tests", Rockwell Aerospace Report, 1995.
3. Johnson, T.F. and Gates, T.S., "Temperature Polyamide Materials in Extreme Temperature Environment", 42nd AIAA/ASME/ASCE/AHS/ASC Structural Dynamics and Materials Conference, Seattle, WA, 2001.
4. GENOA, Progressive Failure Analysis for 2D/3D Laminate/Woven/Braided/ Stitched Polymer and Ceramic Matrix Composite, Software Package, Ver. 3.2, Alpha Star Corporation, Long Beach, CA, 2004.
5. Murthy, P.L.N, and Chamis, C.C, "ICAN: Integrated Composites Analyzer," Journal of Composites Technology & Research, 1986/vol. 24, No.! 1, pp. 1872-1873.
6. Minnetyan, L., Chamis, C.C., and Abdi, F., "Damage Tolerance of Fiber Composite Airfoils with Piezoelectric Adaptive Control System", AIAA 2000-1504, 2000.