Several methods compared with respect to accuracy, design conservatism, and cost. Objective of survey: reduce time and expense of load calculation by selecting approximate method having sufficient accuracy for problem at hand. Methods generally applicable to dynamic load analysis in other aerospace and other vehicle/payload systems.
Methods for Estimating Payload/Vehicle Design Loads
NASA Tech Briefs ; 7 , 4
01.10.1983
Sonstige
Keine Angabe
Englisch
Scientific ballooning payload termination loads
Elsevier | 1992
|Scientific ballooning payload termination loads
NTRS | 1993
|Structural Dynamics Payload Loads Estimates
NTIS | 1981
|Structural dynamics payload loads estimates
NTRS | 1981
|Loads environment for payload/cargo integration
AIAA | 1983
|