3 AC15 DAS202 output

0457-EX-CN-2019 Text Documents

Aerospace Corporation, The

2019-06-10ELS_231831

04 30 2019; 17:51:49PM DAS Application Started 04 30 2019; 17:51:51PM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC15\ 04 30 2019; 17:51:59PM Processing Requirement 4.3-1: Return Status : Not Run ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== 04 30 2019; 17:52:01PM Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== 04 30 2019; 17:52:03PM Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== 04 30 2019; 17:52:06PM Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = AC15 Space Structure Type = Payload Perigee Altitude = 500.000000 (km) Apogee Altitude = 500.000000 (km) Inclination = 51.600000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.033661 (m^2/kg) Start Year = 2020.000000 (yr) Initial Mass = 3.674000 (kg) Final Mass = 3.674000 (kg) Duration = 1.000000 (yr) Station-Kept = False Abandoned = True PMD Perigee Altitude = -1.000000 (km) PMD Apogee Altitude = -1.000000 (km) PMD Inclination = 0.000000 (deg) PMD RAAN = 0.000000 (deg) PMD Argument of Perigee = 0.000000 (deg) PMD Mean Anomaly = 0.000000 (deg)

**OUTPUT** Collision Probability = 0.000000 Returned Error Message: Normal Processing Date Range Error Message: Normal Date Range Status = Pass ============== =============== End of Requirement 4.5-1 =============== 04 30 2019; 17:52:10PM Requirement 4.5-2: Compliant 04 30 2019; 17:52:11PM Processing Requirement 4.6 Return Status : Passed ============== Project Data ============== **INPUT** Space Structure Name = AC15 Space Structure Type = Payload Perigee Altitude = 500.000000 (km) Apogee Altitude = 500.000000 (km) Inclination = 51.600000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.033661 (m^2/kg) Start Year = 2020.000000 (yr) Initial Mass = 3.674000 (kg) Final Mass = 3.674000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 460.328424 (km) PMD Apogee Altitude = 478.918379 (km) PMD Inclination = 51.596252 (deg) PMD RAAN = 56.379706 (deg) PMD Argument of Perigee = 109.354795 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 460.328424 (km) Suggested Apogee Altitude = 478.918379 (km) Returned Error Message = Passes LEO reentry orbit criteria.

Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== 04 30 2019; 17:52:15PM *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AC15 quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 3.674000 Thermal Mass = 3.674000 Diameter/Width = 0.110200 Length = 0.340500 Height = 0.103000 name = Full Body quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.770000 Thermal Mass = 0.010000 Diameter/Width = 0.110200 Length = 0.340500 Height = 0.103000 name = Base Plate quantity = 1 parent = 2 materialID = 8 type = Box Aero Mass = 0.300000 Thermal Mass = 0.300000 Diameter/Width = 0.102300 Length = 0.340500 Height = 0.016700 name = U Frame

quantity = 1 parent = 2 materialID = 8 type = Box Aero Mass = 0.460000 Thermal Mass = 0.460000 Diameter/Width = 0.103000 Length = 0.340500 Height = 0.099000 name = Zenith Lid quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.386000 Thermal Mass = 0.075000 Diameter/Width = 0.103500 Length = 0.110200 Height = 0.008000 name = Antenna (Zenith) quantity = 2 parent = 5 materialID = 40 type = Box Aero Mass = 0.011000 Thermal Mass = 0.011000 Diameter/Width = 0.038100 Length = 0.039900 Height = 0.003200 name = STIM 210 IMU quantity = 1 parent = 5 materialID = 8 type = Box Aero Mass = 0.115000 Thermal Mass = 0.115000 Diameter/Width = 0.048300 Length = 0.064800 Height = 0.025400 name = Sensor Block quantity = 4 parent = 5 materialID = 8 type = Box

Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.015200 Length = 0.044400 Height = 0.009000 name = Star Tracker quantity = 2 parent = 5 materialID = 8 type = Box Aero Mass = 0.055000 Thermal Mass = 0.055000 Diameter/Width = 0.026700 Length = 0.041800 Height = 0.025400 name = Bus Electronics quantity = 7 parent = 1 materialID = 23 type = Box Aero Mass = 0.050000 Thermal Mass = 0.050000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.005000 name = Avionics Bracket quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.090000 Thermal Mass = 0.090000 Diameter/Width = 0.080000 Length = 0.095000 Height = 0.080000 name = Reaction Wheels quantity = 1 parent = 1 materialID = 54 type = Box Aero Mass = 0.255000 Thermal Mass = 0.010000 Diameter/Width = 0.052800 Length = 0.071100

Height = 0.039200 name = Motor with Wheels quantity = 3 parent = 12 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.025000 Length = 0.042400 name = Base quantity = 1 parent = 12 materialID = 8 type = Box Aero Mass = 0.065000 Thermal Mass = 0.065000 Diameter/Width = 0.042800 Length = 0.096800 Height = 0.029200 name = Single Torque Rod quantity = 9 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.018000 Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.078700 name = Battery quantity = 4 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.019000 Length = 0.065000 name = Nadir Lid quantity = 1 parent = 1 materialID = 8 type = Box

Aero Mass = 0.070000 Thermal Mass = 0.070000 Diameter/Width = 0.102600 Length = 0.107700 Height = 0.003200 name = Antenna (Nadir) quantity = 1 parent = 1 materialID = 40 type = Box Aero Mass = 0.015000 Thermal Mass = 0.015000 Diameter/Width = 0.038100 Length = 0.039900 Height = 0.004000 name = Wing Panel quantity = 2 parent = 1 materialID = 23 type = Box Aero Mass = 0.150000 Thermal Mass = 0.150000 Diameter/Width = 0.030000 Length = 0.313500 Height = 0.010000 name = Access Panels quantity = 3 parent = 1 materialID = 8 type = Box Aero Mass = 0.040000 Thermal Mass = 0.040000 Diameter/Width = 0.081900 Length = 0.141400 Height = 0.002000 name = Thermal Strap 1 quantity = 1 parent = 1 materialID = 19 type = Box Aero Mass = 0.064000 Thermal Mass = 0.064000 Diameter/Width = 0.076200 Length = 0.088900

Height = 0.006200 name = Thermal Strap 2 quantity = 1 parent = 1 materialID = 19 type = Box Aero Mass = 0.022000 Thermal Mass = 0.022000 Diameter/Width = 0.039400 Length = 0.041900 Height = 0.002500 name = NFOV Star Tracker quantity = 1 parent = 1 materialID = 8 type = Cylinder Aero Mass = 0.120000 Thermal Mass = 0.120000 Diameter/Width = 0.046000 Length = 0.110000 name = Payload quantity = 1 parent = 1 materialID = 8 type = Cylinder Aero Mass = 0.325000 Thermal Mass = 0.325000 Diameter/Width = 0.060000 Length = 0.134100 name = Laser Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.360000 Thermal Mass = 0.360000 Diameter/Width = 0.082200 Length = 0.141700 Height = 0.020200 name = Context Camera quantity = 1 parent = 1 materialID = 8

type = Cylinder Aero Mass = 0.025000 Thermal Mass = 0.025000 Diameter/Width = 0.030000 Length = 0.034100 **************OUTPUT**** Item Number = 1 name = AC15 Demise Altitude = 77.999691 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Full Body Demise Altitude = 77.969972 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Base Plate Demise Altitude = 75.642285 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = U Frame Demise Altitude = 76.064957 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Demise Altitude = 76.595215 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Antenna (Zenith) Demise Altitude = 75.233996 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = STIM 210 IMU Demise Altitude = 72.510519 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Sensor Block Demise Altitude = 74.620019 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Star Tracker Demise Altitude = 73.193160 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics Demise Altitude = 76.817660 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Avionics Bracket Demise Altitude = 76.777629 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheels Demise Altitude = 75.774293 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Motor with Wheels Demise Altitude = 66.977784 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Base Demise Altitude = 74.146238 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Single Torque Rod Demise Altitude = 73.886316 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Battery Demise Altitude = 69.306824 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Demise Altitude = 76.341832 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Antenna (Nadir) Demise Altitude = 76.172636 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Panel Demise Altitude = 76.329761 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Access Panels Demise Altitude = 77.168136 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thermal Strap 1 Demise Altitude = 76.292058 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thermal Strap 2 Demise Altitude = 76.311824 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = NFOV Star Tracker Demise Altitude = 75.168840 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Payload Demise Altitude = 72.949230 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Laser Assembly Demise Altitude = 72.499261 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Context Camera Demise Altitude = 75.964519 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============


Document Created: 2019-06-07 14:21:18
Document Modified: 2019-06-07 14:21:18
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