Patent ID: 8196858

Claim:
An aircraft configured for flight in an atmosphere having a low density, the aircraft comprising: a fuselage; a pair of wings extending from the fuselage in opposition to one another; a rear stabilizer extending from the fuselage in spaced relationship to the pair of wings; wherein each of the fuselage, the pair of wings, and the rear stabilizer present an upper surface opposing a lower surface; wherein the upper and lower surfaces are defined at an X position along an X-axis in a 3-dimensional X, Y, Z configuration; and wherein the upper and lower surfaces are defined at Y and Z positions along respective Y and Z axes, corresponding substantially to the following table: Y Z 1005.68 117.26 1037.25 437.34 1049.79 117.67 1081.35 438.41 1093.90 118.26 1125.46 438.83 1138.00 119.03 1169.57 438.60 1182.11 119.96 1213.67 437.72 1226.20 121.01 1257.75 436.19 1270.30 122.11 1301.81 434.01 1314.40 123.20 1345.83 431.19 1358.50 124.30 1389.81 427.74 1402.59 125.48 1433.73 423.67 1446.68 126.77 1477.59 419.01 1490.77 128.22 1521.39 413.76 1534.85 129.87 1565.12 407.93 1578.92 131.74 1608.77 401.56 1622.98 133.88 1652.34 394.68 1667.02 136.33 1695.83 387.34 1711.05 139.13 1739.27 379.66 1755.04 142.31 1782.65 371.68 1799.01 145.91 1825.98 363.42 1842.93 149.98 1869.25 354.84 1886.80 154.56 1912.45 345.90 191.27 193.72 1930.61 159.67 1955.57 336.63 195.79 236.57 1974.36 165.31 1998.63 327.04 2018.04 171.45 2041.63 317.21 2061.66 178.05 2084.61 307.28 2105.22 185.01 2127.58 297.33 2148.72 192.28 2170.47 287.02 217.43 159.25 2192.19 199.79 2213.16 275.91 2235.63 207.48 223.69 270.30 2255.58 263.80 2279.04 215.29 2297.80 251.03 2321.20 224.19 257.36 140.96 260.67 294.21 300.44 131.64 300.83 312.40 342.35 327.29 344.24 126.54 3744.64 668.04 3758.76 679.04 3765.49 654.10 3778.09 682.59 3784.17 650.65 3797.57 685.21 3803.05 648.55 3817.10 687.46 3822.01 647.30 3836.67 689.38 3840.99 646.64 384.41 340.58 3856.25 691.10 3859.99 646.44 3875.86 692.61 3878.99 646.57 388.22 123.63 3895.47 694.00 3897.98 647.01 3915.08 695.32 3916.97 647.73 3934.71 696.47 3935.94 648.72 3954.35 697.51 3954.91 649.85 3973.87 651.12 3973.98 698.57 3992.81 652.63 3993.61 699.65 4011.73 654.36 4013.25 700.76 4030.63 656.29 4032.88 701.89 4049.51 658.39 4052.51 703.04 4068.38 660.63 4072.14 704.20 4087.23 662.99 4091.77 705.37 4106.07 665.47 4111.39 706.53 4124.89 668.04 4131.02 707.69 4143.70 670.71 4150.65 708.86 4162.50 673.48 4166.85 699.98 4181.28 676.32 4181.67 687.05 4198.83 681.03 4200.06 679.25 4218.82 682.24 426.85 352.58 432.29 121.80 469.58 363.51 476.39 120.56 512.54 373.55 520.48 119.50 555.68 382.76 564.59 118.60 598.98 391.18 608.69 117.90 642.42 398.84 652.80 117.40 685.98 405.76 696.91 117.05 729.65 411.98 741.02 116.83 773.41 417.53 785.13 116.70 817.25 422.43 829.24 116.66 861.15 426.68 873.35 116.71 905.12 430.30 917.46 116.82 949.13 433.28 961.57 117.00 993.17 435.63.