Satellite Structural Design - Finite Element Analysis for Satellite Structures - page 66

Fig. 3.16 Deformation of preliminary base plate

Fig. 3.17 Stress distribution of preliminary mounting plate

26 9 26 9 26 9 5 9 5 9 5 c.s. for the main eight stringers intended for structure
fastening and load carrying path, L 22 9 22 9 6 9 6 c.s. for the four wall con-
nection corners, and rectangular 4 9 10 mm c.s. for internal and boundary stiffen-
ers. The final F.E.M. for lower frame has no skin and consists of the following beam
cross-sections: channel 22 9 22 9 22 9 4 9 4 9 4 c.s. for the main eight stringers
intended for structure fastening and load carrying path, L 22 9 22 9 6 9 6 c.s. for