"Gulfstream G550 (GV-SP), spec'03. More thrust, improved sfc & aero, evolved from GV. MTOW 91000, OEW 48300, MZFW 54500, MLW 75300. Range 6750nm with 8pax @LRC M0.80 (fuel limited) and NBAA-IFR reserves. Payload-Range lb/nm: 6200/5713, 2106/6658, 0/6862 Range with 8 pax @ M.85 = 6000 nm, @M.87 = 5000 nm. SL-ISA TOFL 5910.ft, Land.dist.2770.ft (flaps 39). Time to FL370 18 mins, to FL410 22 mins." ; File created as Gulfstream G550 ; 17:40:49 on Monday, February 20 2006 ; Parameter Name Value ;Comments aerofoil-clmax 1.35 aerofoil-cm0 -0.05 approach-time 2.5 ;minutes (2.5 minutes) aspect-ratio 7.363 braking-friction 0.5 cabin-aisle-width 0.48 ;metres (18.897638 inches) cabin-altitude 1828.7999 ;metres (5999.9999 feet) cabin-seat-pitch 2.2 ;metres (86.614176 inches) cabin-seat-width 0.635 ;metres (25.000001 inches) cd0-compress.start-mach 0.7 cd0-compressibility-factor 1.15 contingency-fuel-fraction 0 design-cruise-altitude 11887.2 ;metres (39000.001 feet) design-cruise-mach 0.85 dihedral-deg 1 ;degrees (1.0 degrees) dorsal-fin-height-fraction 0.2 dorsal-fin-length-fraction 0.5 eta-u/c 0.1 exist-slats nil exist-winglets t fin-aspect-ratio 0.98 fin-sweep-deg 37 ;degrees (37.0 degrees) fin-t/c 0.095 fin-tailcone-gap 0.18 ;metres (0.5905512 feet) fin-taper 0.65 flap-type :1-slot-fowler front-fuse-length 4.4539813 ;metres (14.6128 feet) front-fuse-name "gulfstream" fuel-density 802.83634 ;kg./cu.metre (6.7 pounds/US.gal.) fuel-vol-adjustment 1.17153 ;cu.metres (309.48546 US.gal.) furnishings-mass-per-pax 272.1552 ;kilograms (599.99999 pounds) fuse-transition 0.15 fuse-width 2.3876 ;metres (7.8333336 feet) ignore-fuel-vol-violations nil landing-flap-deg 39 ;degrees (39.0 degrees) linked-engine-name "Large-bizjet Fan2" mass-per-pax 90.718401 ;kilograms (200.0 pounds) max-landing-mass-ratio 0.8274725 max-operating-altitude 15544.8 ;metres (51000.002 feet) max-payload/design-payload 3.875 mid-fuse-length 11.725656 ;metres (38.470001 feet) mto-mass 41276.872 ;kilograms (90999.999 pounds) nac-length/width 2.75 nac-location-on-fuse 1.65 nac-name "generic2" nac-width 1.8 ;metres (5.905512 feet) nacs-mounted-on-fuse (0.1) number-of-cabin-crew 1 number-of-compressor-stages 16 number-of-flight-crew 3 number-of-pax 8 number-of-windows 14 operational-items-mass 866.2369 ;kilograms (1909.727 pounds) ramp-fuel-allowance 181.4368 ;kilograms (400.0 pounds) rear-fuse-length 9.9802801 ;metres (32.743702 feet) rear-fuse-name "dc9" reference-thrust-per-engine 71171.553 ;newtons (16000.0 pounds-force) required-fin-vol-coeff 0.0407707 required-stab-vol-coeff 0.6118002 roof-top-end 0.45 seats-abreast 2 stab-aspect-ratio 5.05 stab-mounting :high stab-sweep-deg 30 stab-t/c 0.09 stab-tailcone-gap 0 ;metres (0.0 feet) stab-taper 0.41 sweep-deg 27 ;degrees (27.0 degrees) t/c-root 0.1 t/c-tip/root 0.83 takeoff-time 1 ;minutes (1.0 minutes) taper 0.26 taxi-in-time 5 ;minutes (5.0 minutes) taxi-out-time 10 ;minutes (10.0 minutes) user-factor-on-climb-rating 1.1 user-factor-on-continuous-rating 1.14 user-factor-on-cruise-rating 1.1 user-factor-on-induced-drag 0.98 user-factor-on-sfc 0.988 user-factor-on-takeoff-rating 0.9615886 window-depth 0.4826 ;metres (19.000001 inches) window-width 0.6096 ;metres (24.000001 inches) wing-apex-fuse-fraction 0.395 wing-area 105.63076 ;sq.metres (1137.0 sq.feet) wing-transition 0.25 winglet-cant-deg 10 winglet-span/wing-halfspan 0.126 xi-front-spar-root 0.08 xi-front-spar-tip 0.14 xi-rear-spar-root 0.7 xi-rear-spar-tip 0.67 ; Indirectly defined parameters *cruise-altitude-mode* :stepup *cruise-mach-mode* :fixed *flight-levels* (410 450 490 510) *freeze-tail-areas* t *freeze-oew* 21908.493599999998 plane-version 4.1