1968-02-01

Application of Fibrous Composite Materials to Large Rocket Systems 680694

Studies of the potential for minimization of structural weight in large launch vehicles of the future through the use of composite materials are described. Previous structural weight minimization techniques for composites are reviewed and extended. Typical structural efficiency charts are presented. Significant weight saving through the application of an efficiently stiffened composite structure is demonstrated.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
X