3 AC10 DAS202 Output

0827-EX-CN-2018 Text Documents

Aerospace Corporation, The

2018-10-15ELS_218109

10 03 2018; 13:42:15PM DAS Application Started 10 03 2018; 13:45:11PM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC10\ 10 03 2018; 13:45:38PM Processing Requirement 4.3-1: Return Status : Passed ============== Project Data ============== Objects Passing Through LEO = True Number of Objects = 1 **INPUT** Quantity = 29 Final Area-To-Mass Ratio = 0.506300 (m^2/kg) Perigee Altitude = 500.000000 (km) Apogee Altitude = 500.000000 (km) Inclination = 51.600000 (deg) RAAN = -1.000000 (deg) Argument of Perigee = -1.000000 (deg) Mean Anomaly = -1.000000 (deg) Released Year = 2019.000000 (yr) **OUTPUT** Perigee Altitude = -6378.136000 (km) Apogee Altitude = -6378.136000 (km) Inclination = 0.000000 (deg) Lifetime = 0.739726 (yr) Object Reentered within 25 years of Release = True Object-Time = 20.246407 (obj-yrs) Total Object-Time = 20.246407 (obj-yrs) Status = Pass Returned Error Message - Normal Processing ============== =============== End of Requirement 4.3-1 =============== 10 03 2018; 13:45:41PM Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== 10 03 2018; 13:45:43PM Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== 10 03 2018; 13:45:51PM Processing Requirement 4.5-1: Return Status : Passed ==============

Run Data ============== **INPUT** Space Structure Name = AC10A 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 = 0.025188 (m^2/kg) Start Year = 2019.000000 (yr) Initial Mass = 2.590000 (kg) Final Mass = 2.117000 (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 ============== **INPUT** Space Structure Name = AC10B 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 = 0.025119 (m^2/kg) Start Year = 2019.000000 (yr)

Initial Mass = 2.142000 (kg) Final Mass = 2.142000 (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 =============== 10 03 2018; 13:46:32PM Processing Requirement 4.6 Return Status : Passed ============== Project Data ============== **INPUT** Space Structure Name = AC10A 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 = 0.025188 (m^2/kg) Start Year = 2019.000000 (yr) Initial Mass = 2.590000 (kg) Final Mass = 2.117000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 486.678058 (km) PMD Apogee Altitude = 508.295993 (km)

PMD Inclination = 51.599171 (deg) PMD RAAN = 61.771525 (deg) PMD Argument of Perigee = 111.336136 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 486.678058 (km) Suggested Apogee Altitude = 508.295993 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = AC10B 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 = 0.025119 (m^2/kg) Start Year = 2019.000000 (yr) Initial Mass = 2.142000 (kg) Final Mass = 2.142000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 486.220899 (km) PMD Apogee Altitude = 507.610843 (km) PMD Inclination = 51.599099 (deg) PMD RAAN = 61.508446 (deg) PMD Argument of Perigee = 111.076696 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 486.220899 (km) Suggested Apogee Altitude = 507.610843 (km) Returned Error Message = Passes LEO reentry orbit criteria.

Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== 10 03 2018; 13:46:38PM Requirement 4.5-2: Compliant 10 03 2018; 13:46:43PM *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AC10A quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 2.117000 Thermal Mass = 2.117000 Diameter/Width = 0.109000 Length = 0.170000 Height = 0.104000 name = Nadir Lid Assembly-AC10A quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.225000 Thermal Mass = 0.225000 Diameter/Width = 0.100000 Length = 0.100000 Height = 0.017000 name = Reaction Wheel-AC10A quantity = 3 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.004000 Thermal Mass = 0.004000 Diameter/Width = 0.012000 Length = 0.009000 name = Patch Antenna-AC10A quantity = 3

parent = 1 materialID = 40 type = Box Aero Mass = 0.011000 Thermal Mass = 0.011000 Diameter/Width = 0.041000 Length = 0.041000 Height = 0.006000 name = Backplate-AC10A quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.114000 Thermal Mass = 0.114000 Diameter/Width = 0.078000 Length = 0.170000 Height = 0.010000 name = Power Module-AC10A quantity = 1 parent = 1 materialID = 19 type = Box Aero Mass = 0.315000 Thermal Mass = 0.315000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.028000 name = Bus Electronics-AC10A quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.315000 Thermal Mass = 0.315000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.037000 name = Torque Rod-AC10A quantity = 3 parent = 1 materialID = -2 type = Cylinder Aero Mass = 0.018000

Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.079000 name = Walls-AC10A quantity = 3 parent = 1 materialID = 8 type = Box Aero Mass = 0.095000 Thermal Mass = 0.095000 Diameter/Width = 0.078000 Length = 0.170000 Height = 0.010000 name = Wing Assembly-AC10A quantity = 2 parent = 1 materialID = 23 type = Box Aero Mass = 0.057000 Thermal Mass = 0.057000 Diameter/Width = 0.079000 Length = 0.138000 Height = 0.003000 name = Beacon Assembly-AC10A quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.050000 Thermal Mass = 0.050000 Diameter/Width = 0.083000 Length = 0.083000 Height = 0.008000 name = Dispenser Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.600000 Thermal Mass = 0.600000 Diameter/Width = 0.100000 Length = 0.100000 Height = 0.051000

**************OUTPUT**** Item Number = 1 name = AC10A Demise Altitude = 77.994730 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly-AC10A Demise Altitude = 73.137683 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheel-AC10A Demise Altitude = 74.777738 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Patch Antenna-AC10A Demise Altitude = 76.728129 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Backplate-AC10A Demise Altitude = 76.083988 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Power Module-AC10A Demise Altitude = 71.974316 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics-AC10A Demise Altitude = 73.286543 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod-AC10A Demise Altitude = 73.754113 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Walls-AC10A Demise Altitude = 76.392832 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly-AC10A Demise Altitude = 77.140918 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Beacon Assembly-AC10A Demise Altitude = 76.378261 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dispenser Assembly Demise Altitude = 69.325949 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 2 name = AC10B quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 2.142000 Thermal Mass = 2.142000 Diameter/Width = 0.109000 Length = 0.170000 Height = 0.104000 name = Nadir Lid Assembly-AC10B quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.225000

Thermal Mass = 0.225000 Diameter/Width = 0.100000 Length = 0.100000 Height = 0.017000 name = Reaction Wheel-AC10B quantity = 3 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.004000 Thermal Mass = 0.004000 Diameter/Width = 0.012000 Length = 0.009000 name = Patch Antenna-AC10B quantity = 3 parent = 1 materialID = 40 type = Box Aero Mass = 0.011000 Thermal Mass = 0.011000 Diameter/Width = 0.041000 Length = 0.041000 Height = 0.006000 name = Backplate-AC10B quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.114000 Thermal Mass = 0.114000 Diameter/Width = 0.078000 Length = 0.170000 Height = 0.010000 name = Power Module-AC10B quantity = 1 parent = 1 materialID = 19 type = Box Aero Mass = 0.315000 Thermal Mass = 0.315000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.028000

name = Bus Electronics-AC10B quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.315000 Thermal Mass = 0.315000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.072000 name = Torque Rod-AC10B quantity = 3 parent = 1 materialID = -2 type = Cylinder Aero Mass = 0.018000 Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.079000 name = Walls-AC10B quantity = 3 parent = 1 materialID = 8 type = Box Aero Mass = 0.095000 Thermal Mass = 0.095000 Diameter/Width = 0.078000 Length = 0.170000 Height = 0.010000 name = Camera 360 quantity = 1 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.134000 Thermal Mass = 0.134000 Diameter/Width = 0.034000 Length = 0.027000 name = Flux Camera quantity = 1 parent = 1 materialID = 8 type = Cylinder Aero Mass = 0.037000

Thermal Mass = 0.037000 Diameter/Width = 0.031000 Length = 0.022000 name = Wing Assembly-AC10B quantity = 2 parent = 1 materialID = 23 type = Box Aero Mass = 0.057000 Thermal Mass = 0.057000 Diameter/Width = 0.079000 Length = 0.138000 Height = 0.003000 name = Zenith Lid quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.025000 Thermal Mass = 0.025000 Diameter/Width = 0.104000 Length = 0.111000 Height = 0.010000 name = uCPT Box quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.130000 Thermal Mass = 0.130000 Diameter/Width = 0.041000 Length = 0.041000 Height = 0.031000 name = uCPT Vault quantity = 1 parent = 1 materialID = 54 type = Box Aero Mass = 0.024000 Thermal Mass = 0.024000 Diameter/Width = 0.024000 Length = 0.024000 Height = 0.008000

name = uCPT Cover quantity = 1 parent = 1 materialID = 54 type = Box Aero Mass = 0.115000 Thermal Mass = 0.115000 Diameter/Width = 0.041000 Length = 0.041000 Height = 0.024000 name = uCPT Baffles quantity = 8 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.000200 Thermal Mass = 0.000200 Diameter/Width = 0.028000 Length = 0.040000 name = Propulsion Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.163000 Thermal Mass = 0.163000 Diameter/Width = 0.044000 Length = 0.054000 Height = 0.041400 name = uCPT Vault Shield quantity = 1 parent = 1 materialID = -1 type = Box Aero Mass = 0.015000 Thermal Mass = 0.015000 Diameter/Width = 0.024000 Length = 0.024000 Height = 0.002000 **************OUTPUT**** Item Number = 2 name = AC10B Demise Altitude = 77.994871

Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly-AC10B Demise Altitude = 73.165730 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheel-AC10B Demise Altitude = 74.798722 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Patch Antenna-AC10B Demise Altitude = 76.733019 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Backplate-AC10B Demise Altitude = 76.091324 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Power Module-AC10B Demise Altitude = 71.998050 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics-AC10B Demise Altitude = 74.463964 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod-AC10B Demise Altitude = 73.779441 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Walls-AC10B Demise Altitude = 76.398988

Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Camera 360 Demise Altitude = 64.160925 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Flux Camera Demise Altitude = 74.168269 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly-AC10B Demise Altitude = 77.144269 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Demise Altitude = 77.459644 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = uCPT Box Demise Altitude = 71.597011 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = uCPT Vault Demise Altitude = 68.511394 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = uCPT Cover Demise Altitude = 0.000000 Debris Casualty Area = 0.405137 Impact Kinetic Energy = 82.141708 ************************************* name = uCPT Baffles Demise Altitude = 0.000000

Debris Casualty Area = 3.210238 Impact Kinetic Energy = 0.000345 ************************************* name = Propulsion Assembly Demise Altitude = 72.592253 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = uCPT Vault Shield Demise Altitude = 0.000000 Debris Casualty Area = 0.381508 Impact Kinetic Energy = 7.576210 ************************************* ***********INPUT**** Item Number = 3 name = Probe quantity = 29 parent = 0 materialID = 8 type = Box Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.090000 Length = 0.090000 Height = 0.090000 **************OUTPUT**** Item Number = 3 name = Probe Demise Altitude = 77.991879 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============


Document Created: 2018-10-15 17:12:04
Document Modified: 2018-10-15 17:12:04
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