NASA NTRS · 19790007863
Structural Sizing of the EDIN0620 Body Components Using the APAS Structural Synthesis Computer Program
Abstract
The use of a structural synthesis computer program to design components for a heavy lift launch vehicle is defined. A loads program was used to determine the vehicle shears, bending moments, and axial loads at two design loading conditions. A comparison was made between results from the structures program and the results of a weight estimating program which used historical data in determining component weights.
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Nolte, W. E.. 1976-07-01. Structural Sizing of the EDIN0620 Body Components Using the APAS Structural Synthesis Computer Program. https://ntrs.nasa.gov/citations/19790007863
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