The Triplex Destruct System (LCS's on each SRB and on ET) was analyzed for effectiveness for the entire ascent portion of the flight. LSC size/placements were established, LOX/LH2 vent times were predicted, SRB depressurization times were calculated, and SRB/ET/Orbiter structural breakup pattern and times were determined. Further, debris weight and aerodynamic characteristics are presented for use in future hazard analyses. (Author)
Space Shuttle Range Safety Command Destruct System Analysis and Verification. Phase III. Breakup of Space Shuttle Cluster Via Range Safety Command Destruct System
1981
166 pages
Report
No indication
English