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CUVX Design Report - the AOE home page - Virginia Tech

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<strong>CUVX</strong> <strong>Design</strong> – VT Team 2 Page 79boltering aircraft to continue off <strong>the</strong> port side. The lower portion of <strong>the</strong> AEM is angled out at ten degrees tominimize its footprint, saving area on <strong>the</strong> recovery deck.The VLS tubes are located on <strong>the</strong> recovery deck with four tubes on <strong>the</strong> starboard side and four on <strong>the</strong> port sidefor redundancy. The port side tubes are positioned fur<strong>the</strong>r aft than <strong>the</strong> starboard tubes. Refer to Section 4.7 forarrangements of topside sensors and antennas and to Section 4.6.5 for Recovery Deck arrangements.4.10 Weights and Loading4.10.1 WeightsShip weights are grouped by SWBS number. Weights were obtained from manufacturer information, whenpossible, and from ASSET parametrics. Weight values calculated by <strong>the</strong> ship syn<strong>the</strong>sis model are used when noo<strong>the</strong>r values are available. LCGs, TCGs and VCGs for each weight were estimated from machinery and shiparrangements. These centers were used to find moments and <strong>the</strong> lightship COG. A summary of lightship weightsand centers of gravity by SWBS group is listed in Table 41. Weights grouped by SWBS number with centers ofgravity are listed in Appendix D.4.Table 41. Lightship Weight SummarySWBS Group Weight (MT) VCG (m-BL) LCG (m-FP) TCG (m-CL)100 13445 11.29 115.26 0.02200 2179 4.48 118.02 -0.68300 835 14.24 58.40 0.23400 335 17.47 85.73 4.46500 3433 13.75 99.99 -0.61600 1870 14.14 60.35 1.00700 43 24.19 80.00 -10.00Margin 2252 10.77 105.56 0.00Total 24393 11.41 105.70 0.00Figure 72 shows <strong>the</strong> lightship weight distribution curve. It is used with <strong>the</strong> following loading conditions tocalculate still water bending moment.Figure 72. Lightship Weight Distribution for <strong>CUVX</strong>-HI3 (100MT/m)4.10.2 Loading ConditionsTwo loading conditions are considered for <strong>CUVX</strong>: Full Load and Minimum Operating (Minop) as defined inDDS 079-1. The centers of gravity for <strong>the</strong> two loading conditions are calculated using <strong>the</strong> lightship weight andcenter and loads weights and centers. Weights for <strong>the</strong> Full Load condition are estimated with all fuel oil and potablewater tanks filled to 95% and full provisions, general stores, and weapons. The Minimum Operating conditionassumes that all fuel, stores, and weapons are at 33% of <strong>the</strong>ir full load capacity, and that potable water tanks are66% full. Compensated fuel ballast is included in this condition. The full airwing and <strong>the</strong> total weight for <strong>the</strong> creware used in both conditions. A summary of <strong>the</strong> weights for <strong>the</strong> Full Load condition is provided in Table 42, and asummary for <strong>the</strong> Minimum Operating condition is provided in Table 43.4.11 Hydrostatics and StabilityTo assess <strong>the</strong> hydrostatics, intact stability, and damage stability of <strong>CUVX</strong>-HI3, ship offsets are imported intoHECSALV. Hydrostatics are calculated using a range of drafts from 0 to 29 meters. From this information, <strong>the</strong>curves of form, coefficients of form and cross curves are calculated. Using <strong>the</strong> data obtained from <strong>the</strong>secalculations, intact stability is calculated in <strong>the</strong> two loading conditions. The ballast tanks are filled for correct trimand heel. With intact load conditions created and balanced, intact stability and damage stability are examined.

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