CUVX Design Report - the AOE home page - Virginia Tech

CUVX Design – VT Team 2 Page 107rows( PAY)rows( PF20)TRANKW F20n=1 m = 1rows( PAY)rows( PF20)AHULL F20n=1 m = 1rows( PAY)rows( PF20)ADH F20n=1 m = 1if PF20 m1 ,PAY n, PF20 m7 ,, 0 .kWif PF20 m1 ,PAY n, PF20 m4 ,, 0 . ft 2 N . UCAV W .m 2UCAVW 6.4. N . UCAV W . UCAVW 6.4. m 2= 2.744. 10 4 ft 2MTMTif PF20 m1 ,PAY n, PF20 m5 ,, 0 . ft 2AHULL F20 = 2.815. 10 4 ft 26.4. m 2 = 68.88VCD F42 1.5. H HANGDK VCD F42 = 29.528 ftW . F20 VCD F20 W . F42 VCD F42W VP W F20 W F42 VCD VP VCD VP = 33.437 ftW VPW P W VP W P100 W P400 W P500 W P600 W 7W . VP VCD VP W . P100 VCD P100 W . P400 VCD P400 W . P500 VCD P500 W . P600 VCD P600 W . 7VCD 700VCD PW PBATKW PAY BATKW 400 BATKW 500 BATKW 700 BATKW F20 VCD P = 9.883 mTRANKW PAY TRANKW 400 TRANKW 500 TRANKW 700 TRANKW F20 BATKW PAY = 696.54 kWA HPA AHULL 500 AHULL 600 AHULL 700 AHULL F20 A HPA = 2.962. 10 4 ft 2 TRANKW PAY = 636.27 kWA DPA ADH 500 ADH 600 ADH 700 ADH F20 D 10 = 29.624 mVCD F20 = 40.4VCG P100 VCD P100 D 10 VCG P400 VCD P400 D 10 VCG P500 VCD P500 D 10 VCG P600 VCD P600 D 10VCG P VCD P D 10 VCG VP VCD VP D 10 VCG 700 VCD 700 D 10 D 10 = 97.193 ft VCG VP = 63.756 ftPayload Weights and VCG SummaryW P = 2.457. 10 3 lton VCG P = 19.741 mW VP = 2.304. 10 3 lton VCG VP = 63.756 ft (Variable Payload = WF20+WF42)W P100 = 4 lton W P400 = 99.39 lton W P500 = 7.43 lton W P600 = 0 lton W 7= 42.4 ltonVCG P100 = 21.744 m VCG P400 = 24.988 m VCG P500 = 18.803 m VCG P600 = 23.624 m VCG 700 = 24.19 mW F42 = 1.479. 10 3 lton (aircraft fuel) W F20 = 824.976 ltonW F23 = 360.226 lton (aircraft)Payload Area RequirementsRequired payload deck areas in deckhouse: A DPC = 0m 2A DPA = 845.511 m 2In hull: A HPC = 435.437 m 2 A HPA = 2.752. 10 3 m 2Where 'PC' index stands for Command & Surveilance (swbs 400) and 'PA' for armament (swbs 500, 600, 700 and F20).Sonar model (0 for SQR-19 only, 1 for SQS-53C or combination, 2 for SQS-56 or combination): SON TYP = 0Payload Electrical RequirementsBATKW PAY = 696.54 kWTRANKW PAY = 636.27 kW (For winter cruise condition, with sonar)Fin stabilizers: N fins if DP 13, 1, 0 KW fins 0kW . if N fins 0KW fins = 100 kW2d. Endurance parameters and MOPs:E( 12000 . nm) if DP 181( 8000 . nm) if DP 182( 4000.nm) if DP 183VOP 91.0 if DP 181.667 if DP 1820.0 otherwise100. kW otherwiseV e20.kntE = 4. 10 3 nmT S( 120.day) if DP 191( 90.day) if DP 192( 60.day) if DP 193VOP 101.0 if DP 191.7 if DP 1920.0 otherwise2e. CBR Protection and MOP:Collective Protection System : W CPS 60. lton if DP 23130. lton if DP 232VOP 211.0 if DP 231.7 if DP 232W CPS = 60 lton2f. Propulsion System:PSYS TYP 1 if 1 DP 2052 otherwise0.0. lton if DP 233η .98 if 1 DP 205.92 otherwise0.0 if DP 233(Propulsion System Type1 - Mechanical2 - IPSN prop 1 if 1 DP 2031 if 6 DP 209N prop = 2 W AirL W AirSCat if PSYS TYP 1W AirEMALS otherwiseP BPENGTOT2 otherwiseP BPENGTOT = 5.2. 10 4 hpkgSFC ePE = 0.211kW.hr52500. hp if DP 201 DP 20658100. hp if DP 202 DP 20755300. hp if DP 203 DP 20941600. hp if DP 20452000. hp if DP 208 DP 201278800. hp if DP 201087100. hp if DP 201181500. hp if DP 201373300. hp otherwisekgSFC ePE 0.264. if DPkW.hr 201kg0.199. if DPkW.hr 202kg0.202. if DPkW.hr 203kg0.210. if DPkW.hr 204 DP 2014kg0.210. if DPkW.hr 205kg0.261. if DPkW.hr 206kg0.198. if DPkW.hr 207 DP 2011 DP 209kg0.213. if DPkW.hr 208kg0.264. if DPkW.hr 2010 DP 2013kg0.211. otherwisekW.hrkg0.210. = 0.345kW.hr h16.16. m =.4. m 2 =8514. m 3 =122.6. MT =