============================================================================= SOAR Output File: SOAR550.OUT Opt:1 ============================================================================= Computed Engine Propellant Mass = .215 lbs Computed Engine Total Impulse = 27.4 lb-sec _____________________________________________________________________________ Time Thrust Altitude Velocity Acceleration Mass Dyn.Press. Drag sec. lb. feet ft/sec. ft/sec2 lb. lb/ft2 lb. .000 .0 .0 .00 -32.18 3.22 .0 .0 .017 3.9 .0 -.53 6.85 3.22 .0 .0 .033 67.3 -.0 -.42 642.28 3.21 .0 .0 .050 92.9 .1 10.24 901.87 3.20 .1 .0 .066 90.5 .4 25.21 881.10 3.19 .8 .0 .083 95.2 .9 39.84 932.09 3.18 1.9 .0 .100 105.1 1.7 55.31 1036.62 3.16 3.6 .0 .116 110.4 2.8 72.51 1095.29 3.15 6.2 .1 .133 111.8 4.1 90.69 1114.53 3.13 9.8 .1 .149 110.1 5.8 109.19 1101.89 3.12 14.2 .1 .166 109.8 7.7 127.48 1103.50 3.11 19.3 .2 .183 110.8 10.0 145.79 1118.60 3.09 25.2 .2 .199 111.0 12.6 164.35 1125.41 3.08 32.1 .3 .216 108.7 15.5 183.03 1105.88 3.06 39.8 .4 .232 106.9 18.6 201.38 1091.27 3.05 48.2 .5 .249 101.5 22.1 219.49 1038.12 3.03 57.2 .6 .266 90.5 25.9 236.71 924.46 3.02 66.5 .7 .282 73.5 30.0 252.05 745.28 3.01 75.4 .7 .299 42.0 34.3 264.42 409.01 3.00 83.0 .8 .315 6.4 38.7 271.20 27.26 3.00 87.3 .9 .332 .0 43.2 271.46 -41.38 3.00 87.5 .9 .832 .0 173.8 251.12 -40.02 3.00 74.5 .7 1.332 .0 294.4 231.41 -38.82 3.00 63.1 .6 1.832 .0 405.4 212.28 -37.75 3.00 52.9 .5 2.332 .0 506.8 193.65 -36.80 3.00 43.9 .4 2.832 .0 599.1 175.46 -35.96 3.00 35.9 .4 3.332 .0 682.3 157.67 -35.22 3.00 29.0 .3 3.832 .0 756.8 140.22 -34.58 3.00 22.9 .2 4.332 .0 822.6 123.07 -34.03 3.00 17.6 .2 4.832 .0 879.9 106.18 -33.55 3.00 13.1 .1 5.332 .0 928.8 89.51 -33.15 3.00 9.3 .1 5.832 .0 969.5 73.02 -32.82 3.00 6.2 .1 6.332 .0 1001.9 56.68 -32.57 3.00 3.7 .0 6.832 .0 1026.2 40.44 -32.37 3.00 1.9 .0 7.332 .0 1042.3 24.29 -32.25 3.00 .7 .0 7.832 .0 1050.5 8.19 -32.18 3.00 .1 .0 8.332 .0 1050.5 -7.90 -32.17 3.00 .1 .0 8.832 .0 1042.6 -23.97 -32.11 3.00 .7 .0 9.332 .0 1026.6 -40.00 -31.98 3.00 1.8 .0 9.832 .0 1002.6 -55.94 -31.80 3.00 3.6 .0 10.332 .0 970.6 -71.78 -31.55 3.00 6.0 .1 10.832 .0 930.8 -87.48 -31.24 3.00 8.8 .1 11.332 .0 883.2 -103.02 -30.88 3.00 12.3 .1 11.832 .0 827.8 -118.36 -30.47 3.00 16.2 .2 12.332 .0 764.9 -133.47 -30.00 3.00 20.7 .2 12.832 .0 694.4 -148.34 -29.48 3.00 25.6 .3 13.332 .0 616.6 -162.94 -28.91 3.00 31.0 .3 13.832 .0 531.5 -177.25 -28.31 3.00 36.8 .4 14.332 .0 439.4 -191.24 -27.66 3.00 42.9 .4 14.832 .0 340.3 -204.90 -26.98 3.00 49.4 .5 15.332 .0 234.5 -218.21 -26.26 3.00 56.2 .6 15.832 .0 122.2 -231.16 -25.51 3.00 63.3 .6 16.332 .0 3.4 -243.72 -24.75 3.00 70.6 .7 16.832 .0 -121.5 -255.90 -23.95 3.00 78.1 .8 ----------------------------------------------------------------------------- Maximum altitude: 1050.5 feet Maximum velocity: 271.46 feet/sec. Maximum acceleration: 1125.41 feet/sec2 Minimum acceleration: -41.383 feet/sec2 Maximum Mach number : .24 at .33 sec. ============================================================================= ECHO OF INPUT DATA: FILE, RCON550.DAT TITLE, 2" rocket with A-100M KNDX UNITS, ENGLISH STAGES, 1 Cd, .450 DEAD MASS, 3.0000 DIAMETER, 2.0000 FILE, THR550.DAT TITLE, A-100M motor with KNDX propellant UNITS, ENGLISH Isp, 127.000000 TIME STEP, .01660 DATA POINTS, 21 PRINTALL?, Yes THRUST VALUE, 1, .0000 THRUST VALUE, 2, 3.9000 THRUST VALUE, 3, 67.3000 THRUST VALUE, 4, 92.9000 THRUST VALUE, 5, 90.5000 THRUST VALUE, 6, 95.2000 THRUST VALUE, 7, 105.1000 THRUST VALUE, 8, 110.4000 THRUST VALUE, 9, 111.8000 THRUST VALUE, 10, 110.1000 THRUST VALUE, 11, 109.8000 THRUST VALUE, 12, 110.8000 THRUST VALUE, 13, 111.0000 THRUST VALUE, 14, 108.7000 THRUST VALUE, 15, 106.9000 THRUST VALUE, 16, 101.5000 THRUST VALUE, 17, 90.5000 THRUST VALUE, 18, 73.5000 THRUST VALUE, 19, 42.0000 THRUST VALUE, 20, 6.4000 THRUST VALUE, 21, .0000 ****************************** END OF PRINTOUT ******************************