The development of a full scale payload integration method which reduces the cost of a load cycle and is capable of land long very large systems is discussed. The method solves the coupled booster/payload system equations and does not involve additional approximations as compared to the standard transient analysis. The method is cost effective and directly applicable to the shuttle payload design case.
Structural dynamics payload loads estimates
1981-08-01
Report
No indication
English
Scientific ballooning payload termination loads
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|Loads environment for payload/cargo integration
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