Contents: Demonstrate the structural integrity of the missile and missile ducting; Develop a procedure for loading HE-LN2 aboard the missile that is compatible with IOC requirements; Demonstrate the structural integrity of the airborne helium system at high loading rates; Evaluate the Convair propellant loading control system in properly controlling propellant levels in the missile tanks during loading operations; and Develop an integrated propellant loading cycle employing sequences generally compatible with IOC concepts. (Author)


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