============================================================================= SOAR Output File: SOAR721.OUT Opt:1 ============================================================================= Computed Engine Propellant Specific Impulse = 135.7 lb-sec/lb Computed Engine Total Impulse = 435.9 lb-sec _____________________________________________________________________________ Time Thrust Altitude Velocity Acceleration Mass Dyn.Press. Drag sec. lb. feet ft/sec. ft/secı lb. lb/ftı lb. .000 .0 .0 .00 .00 12.32 .0 .0 .175 267.0 .0 .00 675.32 12.14 .0 .0 .351 307.0 8.9 112.76 806.11 11.77 15.1 .3 .526 323.0 41.1 253.90 877.94 11.36 76.5 1.5 .702 340.0 99.1 407.33 956.50 10.94 196.6 4.0 .877 351.0 185.2 574.15 1020.39 10.49 389.6 7.9 1.052 351.0 301.5 751.69 1050.14 10.04 665.5 13.4 1.228 331.0 449.4 933.94 1009.13 9.59 1022.9 20.5 1.403 221.0 628.5 1106.77 598.93 9.24 1429.0 39.8 1.579 44.0 831.5 1205.62 -77.83 9.07 1685.6 56.9 1.754 .0 1041.8 1192.50 -228.52 9.04 1638.9 55.2 1.929 .0 1247.5 1154.08 -208.68 9.04 1525.8 49.6 2.105 .0 1446.9 1119.55 -184.47 9.04 1427.4 42.8 2.280 .0 1640.5 1089.66 -158.54 9.04 1344.5 35.5 2.456 .0 1829.3 1063.43 -141.59 9.04 1273.5 30.7 2.631 .0 2013.7 1039.71 -129.60 9.04 1210.6 27.4 2.806 .0 2194.2 1017.79 -120.77 9.04 1153.9 24.9 2.982 .0 2370.9 997.22 -114.04 9.04 1102.0 23.0 3.157 .0 2544.0 977.70 -108.77 9.04 1053.8 21.5 3.333 .0 2713.9 959.00 -104.55 9.04 1008.8 20.3 3.508 .0 2880.5 940.98 -101.09 9.04 966.4 19.4 3.683 .0 3044.0 923.51 -98.19 9.04 926.4 18.5 3.859 .0 3204.5 906.50 -95.72 9.04 888.3 17.8 4.034 .0 3362.0 889.92 -93.34 9.04 852.1 17.2 4.210 .0 3516.7 873.76 -90.86 9.04 817.7 16.5 4.385 .0 3668.6 858.03 -88.51 9.04 784.9 15.8 4.560 .0 3817.7 842.71 -86.28 9.04 753.7 15.2 4.736 .0 3964.2 827.76 -84.15 9.04 724.1 14.6 4.911 .0 4108.1 813.18 -82.11 9.04 695.8 14.0 5.087 -50.0 4249.5 798.95 -257.36 9.07 668.8 13.5 5.262 .0 4385.7 754.29 -74.48 9.10 593.7 12.0 5.762 .0 4753.7 718.16 -70.11 9.10 532.2 10.7 6.262 .0 5104.2 684.10 -66.23 9.10 477.8 9.6 6.762 .0 5438.1 651.86 -62.79 9.10 429.5 8.7 7.262 .0 5756.3 621.25 -59.71 9.10 386.4 7.8 7.762 .0 6059.6 592.10 -56.96 9.10 347.7 7.0 8.262 .0 6348.7 564.25 -54.48 9.10 313.0 6.3 8.762 .0 6624.1 537.57 -52.25 9.10 281.7 5.7 9.262 .0 6886.4 511.96 -50.24 9.10 253.5 5.1 9.762 .0 7136.2 487.30 -48.42 9.10 227.9 4.6 10.262 .0 7373.8 463.51 -46.76 9.10 204.7 4.1 10.762 .0 7599.8 440.51 -45.26 9.10 183.6 3.7 11.262 .0 7814.5 418.23 -43.89 9.10 164.4 3.3 11.762 .0 8018.2 396.60 -42.65 9.10 146.9 3.0 12.262 .0 8211.2 375.56 -41.51 9.10 131.0 2.6 12.762 .0 8393.8 355.07 -40.47 9.10 116.4 2.3 13.262 .0 8566.3 335.08 -39.52 9.10 103.1 2.1 13.762 .0 8729.0 315.53 -38.66 9.10 91.0 1.8 14.262 .0 8881.9 296.41 -37.87 9.10 79.9 1.6 14.762 .0 9025.4 277.65 -37.15 9.10 69.8 1.4 15.262 .0 9159.6 259.24 -36.49 9.10 60.6 1.2 15.762 .0 9284.7 241.15 -35.90 9.10 52.2 1.1 16.262 .0 9400.8 223.34 -35.36 9.10 44.6 .9 16.762 .0 9508.1 205.78 -34.87 9.10 37.8 .8 17.262 .0 9606.7 188.46 -34.43 9.10 31.6 .6 17.762 .0 9696.6 171.35 -34.03 9.10 26.0 .5 18.262 .0 9778.0 154.42 -33.68 9.10 21.1 .4 18.762 .0 9851.1 137.66 -33.37 9.10 16.7 .3 19.262 .0 9915.7 121.05 -33.10 9.10 12.9 .3 19.762 .0 9972.1 104.56 -32.86 9.10 9.6 .2 20.262 .0 10020.3 88.18 -32.66 9.10 6.8 .1 20.762 .0 10060.3 71.90 -32.50 9.10 4.5 .1 21.262 .0 10092.2 55.68 -32.37 9.10 2.7 .1 21.762 .0 10116.0 39.52 -32.27 9.10 1.4 .0 22.262 .0 10131.8 23.40 -32.21 9.10 .5 .0 22.762 .0 10139.4 7.31 -32.18 9.10 .0 .0 23.262 .0 10139.1 -8.78 -32.17 9.10 .1 .0 23.762 .0 10130.6 -24.86 -32.14 9.10 .5 .0 24.262 .0 10114.2 -40.91 -32.07 9.10 1.5 .0 24.762 .0 10089.7 -56.93 -31.97 9.10 2.8 .1 25.262 .0 10057.3 -72.88 -31.84 9.10 4.7 .1 25.762 .0 10016.9 -88.76 -31.68 9.10 6.9 .1 26.262 .0 9968.5 -104.56 -31.49 9.10 9.6 .2 26.762 .0 9912.3 -120.25 -31.27 9.10 12.7 .3 27.262 .0 9848.3 -135.82 -31.02 9.10 16.3 .3 27.762 .0 9776.5 -151.26 -30.73 9.10 20.2 .4 28.262 .0 9697.1 -166.55 -30.42 9.10 24.6 .5 28.762 .0 9610.0 -181.68 -30.08 9.10 29.3 .6 29.262 .0 9515.4 -196.63 -29.72 9.10 34.5 .7 29.762 .0 9413.4 -211.39 -29.33 9.10 40.0 .8 30.262 .0 9304.1 -225.95 -28.91 9.10 45.8 .9 30.762 .0 9187.5 -240.30 -28.47 9.10 52.0 1.0 31.262 .0 9063.8 -254.42 -28.00 9.10 58.5 1.2 31.762 .0 8933.1 -268.30 -27.52 9.10 65.4 1.3 32.262 .0 8795.5 -281.93 -27.01 9.10 72.5 1.5 32.762 .0 8651.2 -295.31 -26.48 9.10 79.9 1.6 33.262 .0 8500.3 -308.41 -25.94 9.10 87.5 1.8 33.762 .0 8342.9 -321.24 -25.37 9.10 95.4 1.9 34.262 .0 8179.1 -333.78 -24.80 9.10 103.6 2.1 34.762 .0 8009.1 -346.03 -24.20 9.10 111.9 2.3 35.262 .0 7833.1 -357.98 -23.60 9.10 120.4 2.4 35.762 .0 7651.2 -369.63 -22.98 9.10 129.1 2.6 36.262 .0 7463.5 -380.96 -22.35 9.10 137.9 2.8 36.762 .0 7270.3 -391.97 -21.71 9.10 146.9 3.0 37.262 .0 7071.6 -402.67 -21.06 9.10 155.9 3.1 37.762 .0 6867.7 -413.04 -20.41 9.10 165.1 3.3 38.262 .0 6658.6 -423.08 -19.75 9.10 174.3 3.5 38.762 .0 6444.6 -432.79 -19.09 9.10 183.6 3.7 39.262 .0 6225.9 -442.17 -18.43 9.10 192.9 3.9 39.762 .0 6002.5 -451.21 -17.76 9.10 202.3 4.1 40.262 .0 5774.7 -459.93 -17.09 9.10 211.6 4.3 40.762 .0 5542.7 -468.31 -16.43 9.10 221.0 4.5 41.262 .0 5306.5 -476.35 -15.76 9.10 230.3 4.6 41.762 .0 5066.4 -484.07 -15.10 9.10 239.5 4.8 42.262 .0 4822.5 -491.46 -14.45 9.10 248.7 5.0 42.762 .0 4575.0 -498.52 -13.80 9.10 257.8 5.2 43.262 .0 4324.0 -505.26 -13.16 9.10 266.9 5.4 43.762 .0 4069.7 -511.68 -12.52 9.10 275.8 5.6 44.262 .0 3812.4 -517.78 -11.89 9.10 284.6 5.7 44.762 .0 3552.0 -523.57 -11.27 9.10 293.3 5.9 45.262 .0 3288.8 -529.06 -10.67 9.10 301.8 6.1 45.762 .0 3023.0 -534.24 -10.07 9.10 310.2 6.3 46.262 .0 2754.7 -539.13 -9.48 9.10 318.4 6.4 46.762 .0 2483.9 -543.73 -8.91 9.10 326.5 6.6 47.262 .0 2211.0 -548.04 -8.34 9.10 334.4 6.7 47.762 .0 1935.9 -552.07 -7.79 9.10 342.1 6.9 48.262 .0 1658.9 -555.83 -7.26 9.10 349.7 7.0 48.762 .0 1380.1 -559.33 -6.73 9.10 357.0 7.2 49.262 .0 1099.7 -562.57 -6.23 9.10 364.1 7.3 49.762 .0 817.6 -565.56 -5.73 9.10 371.1 7.5 50.262 .0 534.1 -568.30 -5.25 9.10 377.8 7.6 50.762 .0 249.4 -570.81 -4.79 9.10 384.3 7.7 51.262 .0 -36.6 -573.09 -4.33 9.10 390.7 7.9 ----------------------------------------------------------------------------- Maximum altitude: 10139.4 feet Maximum velocity: 1205.62 feet/sec. Maximum acceleration: 1050.14 feet/secı Minimum acceleration: -257.363 feet/secı Maximum Mach number : 1.08 at 1.58 sec. ============================================================================= ECHO OF INPUT DATA: FILE, RCON721.DAT TITLE, Actual Cirrus One rocket, with variable drag, Cdo=.35 UNITS, ENGLISH STAGES, 1 Cd:, Standard for ogive nose rocket DEAD MASS, 9.1030 DIAMETER, 3.2500 FILE, THR912.DAT TITLE, Modified Kappa-DX, with tug force from streamer UNITS, ENGLISH Pmass, 3.21200 TIME STEP, .17540 DATA POINTS, 31 PRINTALL?, Yes THRUST VALUE, 1, .0000 THRUST VALUE, 2, 267.0000 THRUST VALUE, 3, 307.0000 THRUST VALUE, 4, 323.0000 THRUST VALUE, 5, 340.0000 THRUST VALUE, 6, 351.0000 THRUST VALUE, 7, 351.0000 THRUST VALUE, 8, 331.0000 THRUST VALUE, 9, 221.0000 THRUST VALUE, 10, 44.0000 THRUST VALUE, 11, .0000 THRUST VALUE, 12, .0000 THRUST VALUE, 13, .0000 THRUST VALUE, 14, .0000 THRUST VALUE, 15, .0000 THRUST VALUE, 16, .0000 THRUST VALUE, 17, .0000 THRUST VALUE, 18, .0000 THRUST VALUE, 19, .0000 THRUST VALUE, 20, .0000 THRUST VALUE, 21, .0000 THRUST VALUE, 22, .0000 THRUST VALUE, 23, .0000 THRUST VALUE, 24, .0000 THRUST VALUE, 25, .0000 THRUST VALUE, 26, .0000 THRUST VALUE, 27, .0000 THRUST VALUE, 28, .0000 THRUST VALUE, 29, .0000 THRUST VALUE, 30, -50.0000 THRUST VALUE, 30, .0000 ****************************** END OF PRINTOUT ******************************