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"Prelim B787-8 (baseline) estimate, autumn'05.
224 pax @ 210 lb/pax, approx 8350 nm @M0.85
MTOW 476000 lb, OEW 239200, MZFW 340000, MLW 365000.
BOL SFC 0.528 @M.85, FL370.
BET 63800 lbf for GENx-64B.
Payload/range (lb/nm) 100800/5450, 18100/9950 0/10400
Approx TOFL(isa+15) 9300 ft, LFL 5000 ft @MLW."
; File created as B787-8 (baseline)
; 10:36:09 on Friday, March 24 2006
; Parameter Name Value ;Comments
approach-time 2 ;minutes (2.0 minutes)
aspect-ratio 10.583288
bypass-ratio 10
cabin-altitude 1828.7999 ;metres (5999.9999 feet)
cabin-floor-location 0.3
cabin-in-front-fuse-fraction 0.4
cabin-in-rear-fuse-fraction 0.4
cd0-compress.start-mach 0.7
cd0-compressibility-factor 1.025
compressibility-method :rr-adjustable
design-cruise-altitude 11277.6 ;metres (37000.001 feet)
design-cruise-mach 0.9
dihedral-deg 6 ;degrees (6.0 degrees)
eta-u/c 0.08
exist-winglets t
fin-aspect-ratio 1.7
fin-cl-limit-at-vmc 0.9
fin-sweep-deg 40 ;degrees (40.0 degrees)
fin-t/c 0.1
fin-tailcone-gap 3.6575999 ;metres (12.0 feet)
fin-taper 0.333
flap-type :1-slot-fowler
front-fuse-length 11.2776 ;metres (37.000001 feet)
front-fuse-name "b787f"
fuel-density 799.24155 ;kg./cu.metre (6.67 pounds/US.gal.)
fuel-vol-adjustment -18.448 ;cu.metres (-4873.446 US.gal.)
furnishings-mass-per-pax 85 ;kilograms (187.39307 pounds)
fuse-depth/width 1.05
fuse-transition 0.05
fuse-width 5.74 ;metres (18.832022 feet)
landing-flap-deg 45 ;degrees (45.0 degrees)
linked-engine-name "Advanced BPR 10"
main-u/c-wheels-per-a/c 8
mass-per-pax 95.254321 ;kilograms (210.0 pounds)
max-landing-mass-ratio 1.0735294
max-operating-altitude 12496.8 ;metres (41000.001 feet)
max-payload/design-payload 2.1428571
mid-fuse-length 24.841199 ;metres (81.499999 feet)
min-static-margin 0.03
mto-mass 215909.79 ;kilograms (475999.99 pounds)
mto-origin-mass 226796.0 ;kilograms (500000.0 pounds)
nac-length/width 1.55
nac-location-ahead-of-wing 1.03
nac-name "a320"
nac-specific-mass 31.738281 ;kg/sq.m (6.4999999 lb/sq.ft)
nac-width 3.6575999 ;metres (12.0 feet)
nacs-mounted-on-wing (0.265)
number-of-pax 224
operational-items-mass 436.83876 ;kilograms (963.06539 pounds)
planform-break-fraction 0.32
planform-break-t.e.-adjustment 0.88
ramp-fuel-allowance 907.18401 ;kilograms (2000.0 pounds)
rear-fuse-length 19.811999 ;metres (64.999999 feet)
rear-fuse-name "b787r"
reference-thrust-per-engine 278013.88 ;newtons (62500.0 pounds-force)
required-fin-vol-coeff 0.0488607
required-stab-vol-coeff 0.9211616
roof-top-end 0.67
seats-abreast 7
stab-sweep-deg 36
stab-t/c 0.1
stab-tailcone-gap 2.7431999 ;metres (9.0 feet)
stab-taper 0.22
sweep-deg 32.2 ;degrees (32.2 degrees)
t/c-break/root 0.7
t/c-root 0.134
t/c-tip/root 0.655
takeoff-flap-deg 10 ;degrees (10.0 degrees)
takeoff-time 1 ;minutes (1.0 minutes)
taper 0.18
taxi-in-time 5 ;minutes (5.0 minutes)
taxi-out-time 10 ;minutes (10.0 minutes)
thickness-break-fraction 0.333
touchdown-speed-ratio 1.25
twist-deg -3 ;degrees (-3.0 degrees)
u/c-length-below-fuse 2.8955999 ;metres (9.5 feet)
user-factor-on-box-mass 0.85
user-factor-on-climb-rating 1.18
user-factor-on-continuous-rating 1.18
user-factor-on-cruise-rating 1.18
user-factor-on-divergence-mach 1.006
user-factor-on-fin-mass 0.85
user-factor-on-flap-mass 0.85
user-factor-on-fuse-mass 0.85
user-factor-on-induced-drag 0.97
user-factor-on-landing-clmax 1.05
user-factor-on-sfc 1.028
user-factor-on-stab-mass 0.85
user-factor-on-takeoff-rating 1.0646
user-factor-on-u/c-mass 0.95
wing-apex-fuse-fraction 0.3
wing-area 325.29003 ;sq.metres (3501.3926 sq.feet)
wing-transition 0.06
winglet-cant-deg 90
winglet-root-chord/wing-tip-chord 1
winglet-span/wing-halfspan 0.025
xi-rear-spar-root 0.75
; Indirectly defined parameters
*cruise-altitude-mode* :stepup
*cruise-mach-mode* :fixed
*flight-levels* (370 410)
*alternative-cruise-mach* 0.85
*takeoff-delta-isa* 15.0
*aero-ref-definition* :wimpress
*freeze-tail-areas* t
*freeze-oew* 108499.2064
plane-version 4.1