============================================================================= SOAR Output File: SOAR711.OUT Opt:1 ============================================================================= Computed Engine Propellant Specific Impulse = 108.5 lb-sec/lb Computed Engine Total Impulse = 93.3 lb-sec _____________________________________________________________________________ Time Thrust Altitude Velocity Acceleration Mass Dyn.Press. Drag sec. lb. feet ft/sec. ft/secı lb. lb/ftı lb. .000 3.0 .0 .00 -20.20 8.06 .0 .0 .067 8.0 -.0 -1.35 -.23 8.06 .0 .0 .133 37.0 -.1 -1.36 115.84 8.04 .0 .0 .200 55.0 .0 6.36 188.62 8.01 .0 .0 .267 55.0 .9 18.94 189.53 7.98 .4 .0 .333 56.0 2.6 31.58 194.46 7.95 1.2 .0 .400 57.0 5.1 44.55 199.42 7.91 2.4 .1 .467 58.0 8.5 57.85 204.41 7.88 4.0 .1 .534 58.0 12.8 71.48 205.30 7.84 6.1 .1 .600 58.0 18.1 85.16 206.16 7.81 8.6 .2 .667 58.0 24.2 98.90 206.99 7.77 11.6 .2 .734 59.0 31.2 112.70 211.95 7.73 15.1 .3 .800 58.0 39.2 126.83 208.56 7.70 19.1 .4 .867 57.0 48.2 140.72 205.07 7.66 23.5 .5 .934 56.0 58.0 154.39 201.50 7.63 28.3 .6 1.000 54.0 68.7 167.81 193.61 7.59 33.4 .7 1.067 52.0 80.4 180.71 185.59 7.56 38.7 .8 1.134 49.0 92.8 193.07 173.17 7.53 44.2 .9 1.201 43.0 106.1 204.61 147.71 7.50 49.6 1.1 1.267 41.0 120.1 214.44 139.28 7.48 54.4 1.2 1.334 40.0 134.7 223.72 135.09 7.45 59.2 1.3 1.401 37.0 149.9 232.72 122.18 7.43 64.1 1.4 1.467 35.0 165.7 240.85 113.53 7.41 68.6 1.5 1.534 33.0 182.0 248.41 104.83 7.38 72.9 1.6 1.601 32.0 198.8 255.39 100.45 7.36 77.1 1.6 1.667 30.0 216.1 262.08 91.65 7.35 81.1 1.7 1.734 29.0 233.8 268.18 87.21 7.33 84.9 1.8 1.801 27.0 251.8 273.98 78.34 7.31 88.5 1.9 1.868 27.0 270.3 279.20 78.28 7.29 91.9 2.0 1.934 25.0 289.1 284.41 69.36 7.28 95.3 2.0 2.001 24.0 308.2 289.03 64.85 7.26 98.4 2.1 2.068 22.0 327.6 293.34 55.88 7.25 101.3 2.2 2.134 19.0 347.3 297.06 42.46 7.24 103.8 2.2 2.201 16.0 367.2 299.89 29.02 7.22 105.7 2.3 2.268 13.0 387.3 301.82 15.60 7.22 107.0 2.3 2.334 10.0 407.5 302.86 2.19 7.21 107.7 2.3 2.401 7.0 427.7 303.00 -11.19 7.20 107.7 2.3 2.468 4.0 447.9 302.26 -24.53 7.20 107.1 2.3 2.968 .0 593.7 281.42 -41.00 7.20 92.5 2.0 3.468 .0 729.4 261.23 -39.75 7.20 79.4 1.7 3.968 .0 855.1 241.64 -38.63 7.20 67.7 1.4 4.468 .0 971.1 222.58 -37.64 7.20 57.2 1.2 4.968 .0 1077.7 203.99 -36.75 7.20 47.9 1.0 5.468 .0 1175.2 185.81 -35.96 7.20 39.6 .8 5.968 .0 1263.6 168.01 -35.26 7.20 32.3 .7 6.468 .0 1343.2 150.54 -34.65 7.20 25.9 .6 6.968 .0 1414.2 133.35 -34.11 7.20 20.3 .4 7.468 .0 1476.6 116.42 -33.65 7.20 15.4 .3 7.968 .0 1530.7 99.69 -33.25 7.20 11.3 .2 8.468 .0 1576.4 83.15 -32.92 7.20 7.8 .2 8.968 .0 1613.8 66.76 -32.66 7.20 5.1 .1 9.468 .0 1643.1 50.48 -32.45 7.20 2.9 .1 9.968 .0 1664.3 34.30 -32.30 7.20 1.3 .0 10.468 .0 1677.4 18.17 -32.21 7.20 .4 .0 10.968 .0 1682.5 2.08 -32.18 7.20 .0 .0 11.468 .0 1679.5 -14.01 -32.15 7.20 .2 .0 11.968 .0 1668.5 -30.07 -32.08 7.20 1.0 .0 12.468 .0 1649.5 -46.08 -31.95 7.20 2.4 .1 12.968 .0 1622.4 -62.00 -31.76 7.20 4.4 .1 13.468 .0 1587.5 -77.83 -31.52 7.20 6.9 .1 13.968 .0 1544.6 -93.52 -31.23 7.20 9.9 .2 14.468 .0 1494.0 -109.05 -30.88 7.20 13.5 .3 14.968 .0 1435.6 -124.39 -30.49 7.20 17.6 .4 15.468 .0 1369.6 -139.53 -30.05 7.20 22.2 .5 15.968 .0 1296.1 -154.44 -29.57 7.20 27.3 .6 16.468 .0 1215.2 -169.10 -29.05 7.20 32.8 .7 16.968 .0 1127.1 -183.48 -28.48 7.20 38.7 .8 17.468 .0 1031.8 -197.57 -27.88 7.20 45.0 1.0 17.968 .0 929.6 -211.35 -27.25 7.20 51.7 1.1 18.468 .0 820.5 -224.81 -26.58 7.20 58.6 1.3 18.968 .0 704.8 -237.93 -25.89 7.20 65.9 1.4 19.468 .0 582.6 -250.69 -25.17 7.20 73.4 1.6 19.968 .0 454.2 -263.09 -24.43 7.20 81.2 1.7 20.468 .0 319.6 -275.12 -23.67 7.20 89.1 1.9 20.968 .0 179.1 -286.76 -22.90 7.20 97.2 2.1 21.468 .0 32.9 -298.02 -22.11 7.20 105.4 2.3 21.968 .0 -118.8 -308.87 -21.32 7.20 113.8 2.4 ----------------------------------------------------------------------------- Maximum altitude: 1682.5 feet Maximum velocity: 303.00 feet/sec. Maximum acceleration: 211.95 feet/secı Minimum acceleration: -41.002 feet/secı Maximum Mach number : .29 at 22.47 sec. ============================================================================= ECHO OF INPUT DATA: FILE, RCON711.DAT TITLE, Ze-2 flight prediction with Epoch motor and PFC RN UNITS, ENGLISH STAGES, 1 Cd, .450 DEAD MASS, 7.2000 DIAMETER, 2.9500 FILE, THR711.DAT TITLE, Epoch motor with PFC grain RNX-73 Ze-2 UNITS, ENGLISH Pmass, .86000 TIME STEP, .06670 DATA POINTS, 38 PRINTALL?, Yes THRUST VALUE, 1, 3.0000 THRUST VALUE, 2, 8.0000 THRUST VALUE, 3, 37.0000 THRUST VALUE, 4, 55.0000 THRUST VALUE, 5, 55.0000 THRUST VALUE, 6, 56.0000 THRUST VALUE, 7, 57.0000 THRUST VALUE, 8, 58.0000 THRUST VALUE, 9, 58.0000 THRUST VALUE, 10, 58.0000 THRUST VALUE, 11, 58.0000 THRUST VALUE, 12, 59.0000 THRUST VALUE, 13, 58.0000 THRUST VALUE, 14, 57.0000 THRUST VALUE, 15, 56.0000 THRUST VALUE, 16, 54.0000 THRUST VALUE, 17, 52.0000 THRUST VALUE, 18, 49.0000 THRUST VALUE, 19, 43.0000 THRUST VALUE, 20, 41.0000 THRUST VALUE, 21, 40.0000 THRUST VALUE, 22, 37.0000 THRUST VALUE, 23, 35.0000 THRUST VALUE, 24, 33.0000 THRUST VALUE, 25, 32.0000 THRUST VALUE, 26, 30.0000 THRUST VALUE, 27, 29.0000 THRUST VALUE, 28, 27.0000 THRUST VALUE, 29, 27.0000 THRUST VALUE, 30, 25.0000 THRUST VALUE, 31, 24.0000 THRUST VALUE, 32, 22.0000 THRUST VALUE, 33, 19.0000 THRUST VALUE, 34, 16.0000 THRUST VALUE, 35, 13.0000 THRUST VALUE, 36, 10.0000 THRUST VALUE, 37, 7.0000 THRUST VALUE, 38, 4.0000 ****************************** END OF PRINTOUT ******************************