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.
Composite reinforced propellant tanks
1975-02-01
Report
No indication
English
Composite Reinforced Propellant Tanks
NTIS | 1975
|COMPOSITE OVERWRAP POSITIVE EXPULSION PROPELLANT TANKS
British Library Conference Proceedings | 1990
|AIAA | 1992
|Propellant Condensation Prediction in Tanks
British Library Online Contents | 1997
|Propellant management in toroidal tanks
AIAA | 1985
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