M22010 – Structural Applications of the Finite Element Method

TweetShareSharePin0 SharesM22010 – Structural Applications of the Finite Element Method Group Coursework BackgroundIn a space mission the payload is located in the upper part of the launcher inside the fairing; atypical example of payload is a satellite.The satellite is interfaced with the launcher via a Payload Adapter Systems (PAS). The PAS hasthe shape of a…

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