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
Structural Dynamics Payload Loads Estimates
NTIS | 1981
|Structural dynamics payload loads estimates: User guide
NTRS | 1982
|Structual Dynamics Payload Loads Estimates: User Guide
NTIS | 1982
|Scientific ballooning payload termination loads
Elsevier | 1992
|Scientific ballooning payload termination loads
NTRS | 1993
|