A summary of the in-flight mechanical environments of payloads on various Ariane launches is presented. The results obtained from the initial Ariane 4 launch are analyzed and compared to mathematical predictions. The low frequency domain is given priority in reviewing different, payload distribution possibilities. Satellite launching projects are analyzed in terms of load and stiffness limits. Dimensioning procedures are outlined.
Environnement Mecanique en Vol sur les Charges Utiles Mises en Orbite Par les Lanceurs Arianes (Flight-Mechanical Environment on Ariane Launch Vehicle Payloads)
1989
14 pages
Report
No indication
English
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