Jan 28, 2022 #1 sarclee Mechanical Jan 14, 2022 105 For a satellite subsystem loading, can I just use the acceleration profile from the launcher user's manual for analysis which is for the whole satellite?
For a satellite subsystem loading, can I just use the acceleration profile from the launcher user's manual for analysis which is for the whole satellite?
Jan 28, 2022 #2 IRstuff Aerospace Jun 3, 2002 44,773 No. It needs to be propagated by the satellite structure; otherwise you wind up overdesigning, or overstressing TTFN (ta ta for now) I can do absolutely anything. I'm an expert! https://www.youtube.com/watch?v=BKorP55Aqvgfaq731-376 forum1529 Entire Forum list http://www.eng-tips.com/forumlist.cfm Upvote 0 Downvote
No. It needs to be propagated by the satellite structure; otherwise you wind up overdesigning, or overstressing TTFN (ta ta for now) I can do absolutely anything. I'm an expert! https://www.youtube.com/watch?v=BKorP55Aqvgfaq731-376 forum1529 Entire Forum list http://www.eng-tips.com/forumlist.cfm
Feb 2, 2022 Thread starter #3 sarclee Mechanical Jan 14, 2022 105 Thanks IRstuff! I can extract the dynamic response for dynamic analysis... I have not tried to extract any output for static analysis... Upvote 0 Downvote
Thanks IRstuff! I can extract the dynamic response for dynamic analysis... I have not tried to extract any output for static analysis...
