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CUVX Design Report - the AOE home page - Virginia Tech

CUVX Design Report - the AOE home page - Virginia Tech

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<strong>CUVX</strong> <strong>Design</strong> – VT Team 2 Page 116C BT C BTFS if HullForm 1LWLC BTLPD if HullForm 5Cbtmin DP .( Cbtmax Cbtmin)5o<strong>the</strong>rwiseNCbt 1L . FS R FS if HullForm 1BB . FS R FS if HullForm 1C M C XCN = 46.723TT . FS R FS if HullForm 1C BTUS if HullForm 2L . US R US if HullForm 2L LPD if HullForm 53 W FL100. o<strong>the</strong>rwiseC ∆LVA X C . X B. FLT C BLWL. B.TB . US R US if HullForm 2B LPD if HullForm 5C . BT V FLo<strong>the</strong>rwiseC . P C . X LWLC W C WFS if HullForm 1C WUS if HullForm 2C WLPD if HullForm 5T . US R US if HullForm 2T LPD if HullForm 5V FLC . P C . X LWL . o<strong>the</strong>rwiseBD 10 D LPD if HullForm 5LWLo<strong>the</strong>rwiseC D100.278 0.836. C P o<strong>the</strong>rwiseLWLLWL = 213.295 m B = 29.048 m T = 7.02 m D 10 = 29.624 m A X = 195.516 m 2B= 7.343C P = 0.7 C X = 0.95 C ∆L = 86 lton C BT = 4.1 C D10 = 7.2 C vd = 0.105 C B = 0.665 C W = 0.863Balance Check:ft 3Required/Minimal Available ErrorWeight: W T = 2.967. 10 4 MTW FL = 2.994. 10 4 MT ERR = 9.201.10 3Arrangeable area: A TR = 2.073. 10 4 m 2A TA = 1.759. 10 4 m 2 ERR A = 0.152Hangar Area: A HangarReq = 9.322. 10 3 m 2 A HANGmax = 1.203. 10 4 m 2Deckhouse area: A DR = 972.337 m 2A DA = 1.022. 10 3 m 2 V D C . vd V FL V D = 1.082. 10 5 ft 3Propulsion power: P IREQ = 3.949. 10 4 hpP IPRP = 3.637. 10 4 hp N T = 898Electrical plant: KW GREQmech = 0kWKW G = 2.5. 10 3 kWV airweap AHULL . F20 H DKMach. box height: H MBreq = 7.59 mH MB = 10.624 mV airweapWDepth: D airweap10MIN = 26.59 mD 10 = 29.624 m6.4. m2 . HSustained Speed: V MT DKe = 20 kntV S 20. . kntStability: .07-.2 C GMB = 0.086Length of Flight Deck: L FltReq = 100 mL Flt = 159.971 mBreadth of Flight Deck: B FltReq = 25 mB = 29.048 mModule 10 - SIMPLIFIED COST MODELV airweap = 7.846. 10 3 m 3W airweap = 408.655 MTMdol coul Bdol 1000. Mdol KdolMdoldolKdoli1 1, 2..7W F42 = 1.503. 10 3 MT10001000Costed Military Payload: (helo and helo fuel weight not included) V AF = 1.884. 10 3 m 3W MP W 4W 7 W IC W F20 W F23 W MP = 695.755 lton10a. Inflation:Base Year: Y B 2005 iy 1..Y B 1981Average Inflation Rate (%): (from 1981-2005) R I 2.3 F IR I110010b. Lead Ship Cost:iyLead Ship Cost - Shipbuilder Portion:SWBS costs: (See Enclosure 1 for K N factors); includes escalation estimateK N4.8.MdolStructure: K N11.0.Mdol+ Propulsion: K N21.0.Mdol+ Electric: K N3lton .772 C L1 .03395 F Ihp .808 C L2 .00186 F Ilton .91 C L3 .07505 F I+ Command, Control, Surveillance: (less payload GFM cost)2.0.Mdollton .617 . ( CManShip CManAir )C L42.0.Mdol+ Auxiliary: K N5lton .782 . ( CManShip CManAir )F I = 1.726. . K . .772N1 W 1C L1 = 71.262 Mdol. . K . .808N2 P BPENGTOT C L2 = 20.752 Mdol. . K . .91N3 W 3C L3 = 58.185 Mdol.10857. F . I K . .617N4 W 4C L4 = 6.705 MdolC L5.09487. F . I K . .782N5 W 5C L5 = 94.11 Mdol1.0.Mdol+ Outfit: K N6lton .784 C L6 .09859. F . I K . .784N6 W 6C L6 = 61.738 Mdol+ Armament: (Less payload GFM cost)1.0.MdolK N7Clton .987 L7 .00838. F . I K . .987N7 W 7 C L7 = 0.583 MdolW M24+ Margin Cost: C . LM CW LS W Li1 C LM = 31.278 MdolM24i1+ Integration/Engineering: (Lead ship includes detail design engineering and plans for class)K N82. . MdolMdolif HullForm 5 KMdol 1.099 N8 = 10CMdol 1.099 L8 .034.K . N8 C Li1i11.099C LM C L8 = 208.932 Mdolo<strong>the</strong>rwiseMdol 1.09910. . Mdol+ Ship Assembly and Support: (Lead ship includes all tooling, jigs, special facilities for class)K N9.5.MdolMdolif HullForm 5 K( Mdol) N9 = 2C( Mdol) L9 .135.K . N9 C Li1i1.839C LM C L9 = 36.323 Mdol( Mdol) o<strong>the</strong>rwise 2. . Mdol= Total Lead Ship Construction Cost: (BCC):C LCCC Li1 C L8 C L9 C LM C LCC = 589.868 Mdoli1

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