NASA NTRS · 19750013268
Composite reinforced propellant tanks
Abstract
Design studies involving weight and cost were carried out for several structural concepts applicable to space shuttle disposable tankage. An effective design, a honeycomb stabilized pressure vessel, was chosen. A test model was designed and fabricated.
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Brown, L. D., Martin, M. J., Aleck, B. J., Landes, R.. 1975-02-01. Composite reinforced propellant tanks. https://ntrs.nasa.gov/citations/19750013268
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