111. Structural Design Considerations for a High Altitude Sounding Rocket of the Viking Type
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Paper
Abstract
As well as growth in the fields of propulsion, electronics and aerodynamics, progress in rocket design must include development of structural materials and techniques. The task of the structures engineer is that of continuous improvement in mass ratio by reduction of rocket weight empty. Accomplishment of this task should be limited only by compatibility with other systems in the rocket and with operational requirements.
A brief summary is made of the structural design considerations necessary prior to the flight of a high altitude sounding rocket of the Viking type. Several problems in need of immediate solution are mentioned in conclusion.