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Exploring the Unknown: Selected Documents in ... - The Black Vault

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<strong>Explor<strong>in</strong>g</strong> <strong>the</strong> <strong>Unknown</strong> 101<br />

5.1.2.2 Ultimate strength – Failure shall not occur under design ultimate loads.<br />

Excessive leakage of <strong>the</strong> pressure capsule under ultimate load is considered<br />

as a failure.<br />

5.1.2.3 Temperature – <strong>The</strong> effects of <strong>the</strong> temperature on load<strong>in</strong>g conditions and<br />

allowable stresses shall be considered where <strong>the</strong>rmal effects are significant.<br />

5.1.3 Load<strong>in</strong>g types - <strong>The</strong> follow<strong>in</strong>g types of loads are to be considered for all<br />

load<strong>in</strong>g conditions:<br />

5.1.3.1 Aerodynamic Loads<br />

5.1.3.1.1 Maneuver (static – dynamic)<br />

5.1.3.1.2 Gust<br />

5.1.3.1.3 W<strong>in</strong>d shear<br />

5.1.3.1.4 Buffet<strong>in</strong>g<br />

5.1.3.1.5 Flutter<br />

5.1.3.2 Inertial loads<br />

[14]<br />

5.1.3.3 Impact loads (water and land)<br />

5.1.3.4 Loads or stresses <strong>in</strong>duced by vibration <strong>in</strong>clud<strong>in</strong>g noise effects<br />

5.1.3.5 Loads or stresses <strong>in</strong>duced by heat<strong>in</strong>g<br />

5.1.4 Load<strong>in</strong>g conditions - <strong>The</strong> follow<strong>in</strong>g trajectory phases must be exam<strong>in</strong>ed<br />

for load<strong>in</strong>g conditions.<br />

5.1.4.1 Ground handl<strong>in</strong>g – <strong>The</strong> effect of all ground handl<strong>in</strong>g conditions must<br />

be considered such as <strong>the</strong> strength of fitt<strong>in</strong>gs attached to <strong>the</strong> capsule for<br />

purpose of transmitt<strong>in</strong>g handl<strong>in</strong>g loads to <strong>the</strong> capsule.<br />

5.1.4.2 In-flight conditions<br />

5.1.3.2.1 General – Air loads and <strong>in</strong>ertial loads for all phases of <strong>the</strong> mission shall<br />

be associated with <strong>the</strong> design trajectories with deviations from <strong>the</strong> design<br />

trajectories to be specified by <strong>the</strong> proved statistical reliability of <strong>the</strong> propulsion<br />

and control systems.<br />

In addition, certa<strong>in</strong> specified conditions of malfunction of <strong>the</strong> propulsion<br />

and control systems shall be considered specified. <strong>The</strong> structural<br />

weight penalties associated with <strong>the</strong>se malfunctions shall be assessed.

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