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PRO.LB.0.NT.003.ASC Issue. 6 rev. 3 Page: 3.21<br />

PL - 4.2.5 - 3<br />

The following definitions shall be applied:<br />

Qualification loads = 1.25 x Flight limit loads except for ground handling where:<br />

- qualification loads = 2 x Flight limit loads for nominal analysis and<br />

- qualification loads = 1.5 x limit loads for fail safe analysis (where 1.5 corresponds to the dynamic<br />

factor <strong>du</strong>e to the loss of one handling point).<br />

Sizing loads = JY (or JU) x Qualification loads<br />

The safety margin is defined as follows :<br />

where :<br />

σ admissible<br />

S.<br />

M.<br />

= −1<br />

σ<br />

calculated<br />

the admissible stress is the yield (respectively ultimate) stress when estimating the safety margin wrt yield<br />

(respectively ultimate).<br />

the admissible stress for single points failure pieces of hardware shall be "A" type values (99% probability with<br />

a 95% confidence level),<br />

the admissible stress for re<strong>du</strong>ndant pieces of hardware shall be "B" type values (90% probability with a 95%<br />

confidence level),<br />

the calculated stress is the qualification stress times the yield (respectively ultimate) safety factor.<br />

PL - 4.2.5 - 4 a<br />

All safety margins shall be positive:<br />

• local buckling criterion: there shall be no buckling under qualification loads<br />

4.2.5.3 Notching philosophy<br />

PL - 4.2.5 - 5<br />

Notching at payload level is allowed <strong>du</strong>ring sine vibration test in order not to exceed, at the<br />

platform/payload interface, the Quasi-Static equivalent loads (resultant forces and moments at the<br />

geometrical centre of the interface points) after Satellite Contractor agreement<br />

Notching at payload units level is forbidden.<br />

PL - 4.2.5 - 6<br />

For notching <strong>du</strong>ring random vibration tests, the Payload Supplier shall contact either ALCATEL SPACE or<br />

CNES.<br />

4.2.5.4 Structural mathematical models<br />

The requirements for the quality of mathematical models, numbering ranges and interface point locations are given<br />

in section 4.6.1.<br />

All right reserved. ALCATEL SPACE /CNES<br />

Passing and copying of this <strong>document</strong>, use and communication of its content is not permitted without prior written authorization.

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