3 AC14 DAS202 output

0520-EX-CN-2019 Text Documents

Aerospace Corporation, The

2019-06-26ELS_232993

04 11 2019; 10:31:00AM DAS Application Started 04 11 2019; 10:31:02AM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC14\ 04 11 2019; 10:31:05AM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC14\ 04 11 2019; 10:31:08AM Processing Requirement 4.3-1: Return Status : Not Run ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== 04 11 2019; 10:31:10AM Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== 04 11 2019; 10:31:12AM Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== 04 11 2019; 10:31:16AM Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = AC14 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 = 0.035722 (m^2/kg) Start Year = 2019.000000 (yr) Initial Mass = 3.462000 (kg) Final Mass = 3.462000 (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 11 2019; 10:31:20AM Requirement 4.5-2: Compliant 04 11 2019; 10:31:21AM Processing Requirement 4.6 Return Status : Passed ============== Project Data ============== **INPUT** Space Structure Name = AC14 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 = 0.035722 (m^2/kg) Start Year = 2019.000000 (yr) Initial Mass = 3.462000 (kg) Final Mass = 3.462000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 485.086537 (km) PMD Apogee Altitude = 506.018128 (km) PMD Inclination = 51.598929 (deg) PMD RAAN = 60.883973 (deg) PMD Argument of Perigee = 110.343292 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 485.086537 (km) Suggested Apogee Altitude = 506.018128 (km)

Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== 04 11 2019; 10:31:26AM *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AC14 quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 3.462000 Thermal Mass = 3.462000 Diameter/Width = 0.110200 Length = 0.340500 Height = 0.103000 name = Full Body quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.694000 Thermal Mass = 0.001000 Diameter/Width = 0.110200 Length = 0.340500 Height = 0.103000 name = Body Base Plate quantity = 1 parent = 2 materialID = 8 type = Box Aero Mass = 0.250000 Thermal Mass = 0.250000 Diameter/Width = 0.102800 Length = 0.330100 Height = 0.011200

name = Frame quantity = 1 parent = 2 materialID = 8 type = Box Aero Mass = 0.443000 Thermal Mass = 0.443000 Diameter/Width = 0.103000 Length = 0.330100 Height = 0.099000 name = Nadir Lid Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.442000 Thermal Mass = 0.141000 Diameter/Width = 0.103500 Length = 0.110200 Height = 0.008000 name = Antenna (Nadir) quantity = 1 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 = 0.116000 Thermal Mass = 0.116000 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 = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.627000 Thermal Mass = 0.627000 Diameter/Width = 0.085000 Length = 0.097100 Height = 0.084900 name = Reaction Wheels quantity = 1 parent = 1 materialID = 54 type = Box Aero Mass = 0.256000 Thermal Mass = 0.001000 Diameter/Width = 0.052800 Length = 0.071100 Height = 0.039200 name = Motor with Wheels quantity = 3 parent = 11 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.025000

Length = 0.042400 name = Base quantity = 1 parent = 11 materialID = 8 type = Box Aero Mass = 0.075000 Thermal Mass = 0.075000 Diameter/Width = 0.042800 Length = 0.096800 Height = 0.029200 name = 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 = 0.018000 Length = 0.065000 name = Zenith Lid Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.132000 Thermal Mass = 0.100000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.016700 name = Antenna (Zenith) quantity = 2 parent = 16 materialID = 40

type = Box Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.038100 Length = 0.040000 Height = 0.005000 name = Wing Assembly quantity = 2 parent = 1 materialID = 8 type = Box Aero Mass = 0.148000 Thermal Mass = 0.148000 Diameter/Width = 0.073700 Length = 0.313500 Height = 0.002700 name = Side-Mounted Module quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.115000 Thermal Mass = 0.115000 Diameter/Width = 0.049900 Length = 0.086800 Height = 0.023300 name = CNT Heater quantity = 1 parent = 1 materialID = 27 type = Box Aero Mass = 0.043000 Thermal Mass = 0.043000 Diameter/Width = 0.044500 Length = 0.076200 Height = 0.012700 name = Thermal Strap quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.064000 Thermal Mass = 0.064000 Diameter/Width = 0.076200

Length = 0.088900 Height = 0.006200 name = Deployable Baffle quantity = 1 parent = 1 materialID = 8 type = Cylinder Aero Mass = 0.213000 Thermal Mass = 0.213000 Diameter/Width = 0.095300 Length = 0.056600 name = Paint Experiment quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.001800 Thermal Mass = 0.001800 Diameter/Width = 0.040600 Length = 0.082500 Height = 0.004400 name = CSAC quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.159000 Thermal Mass = 0.159000 Diameter/Width = 0.071100 Length = 0.078700 Height = 0.017200 **************OUTPUT**** Item Number = 1 name = AC14 Demise Altitude = 77.994613 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Full Body Demise Altitude = 77.994613 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Body Base Plate Demise Altitude = 75.829363 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Frame Demise Altitude = 76.078933 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly Demise Altitude = 75.297425 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Antenna (Nadir) Demise Altitude = 73.917222 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = STIM 210 IMU Demise Altitude = 71.080199 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Sensor Block Demise Altitude = 73.315675 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Star Tracker Demise Altitude = 71.873550 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics Demise Altitude = 72.849285 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Reaction Wheels Demise Altitude = 76.982160 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Motor with Wheels Demise Altitude = 67.854722 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Base Demise Altitude = 75.054629 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod Demise Altitude = 73.882894 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Battery Demise Altitude = 69.170441 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Assembly Demise Altitude = 76.095050 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Antenna (Zenith) Demise Altitude = 73.413363 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly Demise Altitude = 76.062840 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Side-Mounted Module Demise Altitude = 74.672957 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = CNT Heater Demise Altitude = 77.570035 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thermal Strap Demise Altitude = 75.927597 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Deployable Baffle Demise Altitude = 73.843511 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Paint Experiment Demise Altitude = 77.914574 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = CSAC Demise Altitude = 73.224886 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============


Document Created: 2019-06-26 16:29:37
Document Modified: 2019-06-26 16:29:37
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