Civil Engineering Reference
In-Depth Information
Fig. 3.18
Deformation of preliminary mounting plate
Fig. 3.19
Stress distribution of preliminary basis plate without struts
the wall connection corners, and rectangular 3 9 10 mm c.s. for internal and
boundary stiffeners. Table
3.2
and Figs.
3.14
,
3.15
,
3.16
,
3.17
,
3.18
,
3.19
,
3.20
,
3.21
,
3.22
,
3.23
,
3.24
,
3.25
,
3.26
,
3.27,
and
3.28
give the final stress and deformation
distributions in the various structural models. It is seen that all structural modules of
Small Sat have acceptable strength and stiffness.
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