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Accession Number:
AD0276713
Title:
FEASIBILITY DEMOSTRATION OF THE DESIGN, FABRICATION AND TESTING OF FILAMENT WOUND FIBERGLASS LIQUID PROPELLANT TANKS
Corporate Author:
BOEING CO SEATTLE WASH
Report Date:
1962-05-01
Abstract:
The report presents discussions and data derived from a program that investigated the feasibility of applying high-strength materials and advanced fabrication techniques to high-pressure, storable, liquid-rocket propellant tankage. The major design goal was to attain minimum weight tankage commensurate with performance requirements. Three 70-inch-diameter 210-inch-long tanks were filament wound with fiberglass yarn and epoxy resin. Author
Pages:
0001
Contract Number:
AF04 611 6006
File Size:
0.00MB
