An analysis of the impact of the Minuteman III Payload Transporter Type III into a nonyielding target at 46 m.p.h. and 30 m.p.h., and into a yielding target at 46 m.p.h. is presented. The analysis considers the structural response of the tiedown system which secures the Minuteman III re-entry system to the floor of the payload transporter. A finite element model of the re-entry system, its tiedown system, which includes tie-rods and shear pins, and the pallet plate which is attached to the transporter floating plate, was constructed. Because accelerations of the payload transporter are not known, acceleration data from one-quarter scale testing of the Safe Secure Trailer was used to investigate the response of the tiedown system. These accelerations were applied to the pallet plate. The ABAQUS computer code was used to predict the forces in the members of the tiedown system. (ERA citation 19:013015)
Impact analysis of Minuteman III Payload Transporter Type III
1993
39 pages
Report
Keine Angabe
Englisch
Engineering Index Backfile | 1963
|Analysis methods and results of digital dynamic analysis of minuteman transporter-erector
Engineering Index Backfile | 1963
|Analysis Methods and Results of Digital Dynamic Analysis of the Minuteman Transporter-Erector
SAE Technical Papers | 1963
|AIAA | 1976
|AIAA | 1975
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