#Name Of Rocket: NOMAD-II #Type of Nose Cone = Conic #Length of Nose Cone = 24.0000 #Diameter of Nose Cone = 8.5000 #Area of Nose Cone = 102.0000 #Centroid of Nose Cone = 16.0000 #BEq Coefficient of Nose = 2.0000 #BEq Centroid of Nose = 16.0000 #Distance to Body Tube = 24.0000 #Length of Body Tube = 99.0000 #Diameter of Body Tube = 8.2500 #Area of Body Tube = 816.7500 #Centroid of Body Tube = 73.5000 #Distance to Xitn (01) = 123.0000 #Length of Transition = 3.5000 #Diameter at Front = 8.2500 #Diameter at Rear = 12.2500 #Area of Transition = 35.8750 #Centroid of Transition = 124.8638 #BEq Coefficient of Xitn = 2.2699 #BEq Centroid of Xitn = 124.8638 #Distance to Xitn (02) = 126.5000 #Length of Transition = 32.0000 #Diameter at Front = 12.2500 #Diameter at Rear = 12.2500 #Area of Transition = 392.0000 #Centroid of Transition = 142.5000 #BEq Coefficient of Xitn = 0.0000 #BEq Centroid of Xitn = 0.0000 #Number of Fins = 3 #Radial Angle of Fins = 120.0000 #Projected Area of a Fin = 199.6395 #Centroid of One Fin = 8.5000 #Distance to Fin Can = 158.5000 #Length of Fin Can = 18.0000 #Total Area of Fin Can = 619.7790 #Centroid of Fin Can = 167.1779 #Root Chord = 17.0000 #Tip Chord = 12.0000 #Sweep Back = 2.5000 #Fin Span = 17.0000 #MidChord Length = 17.0000 #Diameter at Front = 12.2500 #Diameter at Rear = 12.2500 #Aspect Ratio = 2.3448 #Area of Fin = 246.5000, 246.5000 #Centroid of Fin (z,r) = 8.5000, 8.0115 #MidChord Endpoint (z,r) = 8.5000, 17.0000 #BEq Coefficient of Fins = 23.8939 #BEq Centroid of Fins = 163.3391 #Length of Rocket = 175.5000 #Sum of xAreas of Rocket = 225615.9584 #Total Area of Rocket = 1966.4040 #Centroid of Rocket = 114.7353 (-60.7647) #BEq Coefficient, Rocket = 28.1638 #BEq Center of Pressure = 149.7751 (-25.7249) # I Z1[i]+Zf Y1[i]+R Z1[i] Y1[i] #== ========= ========= ======== ========= 1 158.6393 6.1250 0.1393 0.0000 2 161.0000 20.0268 2.5000 13.9018 3 173.0000 20.0268 14.5000 13.9018 4 175.3607 6.1250 16.8607 0.0000 1 158.6393 -6.1250 0.1393 -0.0000 2 161.0000 -20.0268 2.5000 -13.9018 3 173.0000 -20.0268 14.5000 -13.9018 4 175.3607 -6.1250 16.8607 -0.0000 #Fin at Angle 0 1 158.5000 -0.1875 2 158.5000 0.1875 3 175.5000 0.1875 4 175.5000 -0.1875 5 158.5000 -0.1875 #Fin Can Data 2 158.5000 6.1250 3 176.5000 6.1250 4 176.5000 0.1875 6 158.5000 -6.1250 7 176.5000 -6.1250 8 176.5000 -0.1875 #Nose Cone Data 1 0.0000 0.0000 2 2.4000 0.4250 3 4.8000 0.8500 4 7.2000 1.2750 5 9.6000 1.7000 6 12.0000 2.1250 7 14.4000 2.5500 8 16.8000 2.9750 9 19.2000 3.4000 10 21.6000 3.8250 11 24.0000 4.2500 1 0.0000 -0.0000 2 2.4000 -0.4250 3 4.8000 -0.8500 4 7.2000 -1.2750 5 9.6000 -1.7000 6 12.0000 -2.1250 7 14.4000 -2.5500 8 16.8000 -2.9750 9 19.2000 -3.4000 10 21.6000 -3.8250 11 24.0000 -4.2500 12 24.0000 4.2500 #Body Tube Data 1 24.0000 4.1250 2 123.0000 4.1250 3 123.0000 -4.1250 4 24.0000 -4.1250 #Mark The Centroid 1 113.8853 0.0000 2 115.5853 0.0000 1 114.7353 -0.8500 2 114.7353 0.8500 #Mark The CP 1 148.9251 0.0000 2 150.6251 0.0000 1 149.7751 -0.8500 2 149.7751 0.8500 #Transition (1) Data 1 123.0000 4.1250 2 126.5000 6.1250 3 126.5000 -6.1250 4 123.0000 -4.1250 5 123.0000 4.1250 #Transition (2) Data 1 126.5000 6.1250 2 158.5000 6.1250 3 158.5000 -6.1250 4 126.5000 -6.1250 5 126.5000 6.1250 #Single Fins Rotated 90 Degrees # I Z[i]-2Zf Y[i]+2R Z[i] Y[i] #== ========= ========= ======== ========= 1 158.5000 34.0000 0.0000 0.0000 2 161.0000 51.0000 2.5000 17.0000 3 173.0000 51.0000 14.5000 17.0000 4 175.5000 34.0000 17.0000 0.0000 5 158.5000 34.0000 0.0000 0.0000 7 167.0000 34.0000 8.5000 0.0000 Root Midpoint # 8 167.0000 42.0115 8.5000 8.0115 Centroid Of Fin 9 167.0000 51.0000 8.5000 17.0000 Mid Chord Endpoint 1 166.1500 42.0115 2 167.8500 42.0115 1 167.0000 41.1615 2 167.0000 42.8615