4 AC7 DAS202 Output v1

0586-EX-PL-2015 Text Documents

Aerospace Corporation, THE

2015-09-12ELS_167011

09 11 2015; 09:25:18AM DAS Application Started 09 11 2015; 09:25:18AM Opened Project C:\DAS 2.0\aerocube_DAS\ac7_das\ 09 11 2015; 09:25:51AM Processing Requirement 4.6 Return Status : Passed ============== Project Data ============== **INPUT** Space Structure Name = Wing Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.159619 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.055000 (kg) Final Mass = 0.055000 (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** Suggested Perigee Altitude = 450.000000 (km) Suggested Apogee Altitude = 720.000000 (km) Returned Error Message = Reentry during mission (no PMD req.). Released Year = 2017 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Anti-Nadir Lid Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg)

RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.097202 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.058300 (kg) Final Mass = 0.058300 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 432.775622 (km) PMD Apogee Altitude = 590.960502 (km) PMD Inclination = 97.990959 (deg) PMD RAAN = 18.181916 (deg) PMD Argument of Perigee = 204.086193 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 432.775622 (km) Suggested Apogee Altitude = 590.960502 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2018 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Camera Lens (Xenoplan/Schneider) Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.015845 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.087200 (kg) Final Mass = 0.087200 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 453.993371 (km) PMD Apogee Altitude = 697.532721 (km) PMD Inclination = 98.003275 (deg) PMD RAAN = 12.597099 (deg) PMD Argument of Perigee = 225.464815 (deg) PMD Mean Anomaly = 0.000000 (deg)

**OUTPUT** Suggested Perigee Altitude = 453.993371 (km) Suggested Apogee Altitude = 697.532721 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2023 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Rate Gyro Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.029592 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.095000 (kg) Final Mass = 0.095000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 451.643742 (km) PMD Apogee Altitude = 682.741379 (km) PMD Inclination = 98.001548 (deg) PMD RAAN = 13.402918 (deg) PMD Argument of Perigee = 222.460933 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 451.643742 (km) Suggested Apogee Altitude = 682.741379 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2022 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Nadir Lid Assembly Space Structure Type = Payload

Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.031117 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.187000 (kg) Final Mass = 0.187000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 451.364490 (km) PMD Apogee Altitude = 681.046962 (km) PMD Inclination = 98.001350 (deg) PMD RAAN = 13.494819 (deg) PMD Argument of Perigee = 222.117077 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 451.364490 (km) Suggested Apogee Altitude = 681.046962 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Laser Comm Plate Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.032464 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.220700 (kg) Final Mass = 0.220700 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 451.114221 (km) PMD Apogee Altitude = 679.539377 (km) PMD Inclination = 98.001175 (deg) PMD RAAN = 13.576510 (deg)

PMD Argument of Perigee = 221.811196 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 451.114221 (km) Suggested Apogee Altitude = 679.539377 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Laser Isolator Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.007987 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.227000 (kg) Final Mass = 0.227000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 455.215519 (km) PMD Apogee Altitude = 705.628070 (km) PMD Inclination = 98.004223 (deg) PMD RAAN = 12.153692 (deg) PMD Argument of Perigee = 227.109749 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 455.215519 (km) Suggested Apogee Altitude = 705.628070 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2025 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT**

Space Structure Name = Body Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.052167 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.450000 (kg) Final Mass = 0.450000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 447.035307 (km) PMD Apogee Altitude = 656.333218 (km) PMD Inclination = 97.998481 (deg) PMD RAAN = 14.823596 (deg) PMD Argument of Perigee = 217.112531 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 447.035307 (km) Suggested Apogee Altitude = 656.333218 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = Electronics module with batteries Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.017121 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.514000 (kg) Final Mass = 0.514000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 453.787175 (km)

PMD Apogee Altitude = 696.194944 (km) PMD Inclination = 98.003118 (deg) PMD RAAN = 12.670224 (deg) PMD Argument of Perigee = 225.193017 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 453.787175 (km) Suggested Apogee Altitude = 696.194944 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2022 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = AC7 Propulsion Unit Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.044400 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.131000 (kg) Final Mass = 0.131000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 448.745033 (km) PMD Apogee Altitude = 665.759406 (km) PMD Inclination = 97.999574 (deg) PMD RAAN = 14.319552 (deg) PMD Argument of Perigee = 219.018518 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 448.745033 (km) Suggested Apogee Altitude = 665.759406 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ==============

**INPUT** Space Structure Name = AeroCube7 complete Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.008000 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 2.500000 (kg) Final Mass = 2.500000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 455.213589 (km) PMD Apogee Altitude = 705.615059 (km) PMD Inclination = 98.004221 (deg) PMD RAAN = 12.154406 (deg) PMD Argument of Perigee = 227.107105 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 455.213589 (km) Suggested Apogee Altitude = 705.615059 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2025 (yr) Requirement = 61 Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== 09 11 2015; 09:25:59AM Processing Requirement 4.3-1: Return Status : Not Run ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== 09 11 2015; 09:26:31AM Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available =====================

=============== End of Requirement 4.3-2 =============== 09 11 2015; 09:26:46AM Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== 09 11 2015; 09:27:08AM Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = Wing Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.159619 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.055000 (kg) Final Mass = 0.055000 (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 = Anti-Nadir Lid Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg)

Final Area-To-Mass Ratio = 0.097202 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.058300 (kg) Final Mass = 0.058300 (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 = Camera Lens (Xenoplan/Schneider) Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.015845 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.087200 (kg) Final Mass = 0.087200 (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 = Rate Gyro Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.029592 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.095000 (kg) Final Mass = 0.095000 (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 = Nadir Lid Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.031117 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.187000 (kg) Final Mass = 0.187000 (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 = Laser Comm Plate Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.032464 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.220700 (kg) Final Mass = 0.220700 (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 = Laser Isolator Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg)

RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.007987 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.227000 (kg) Final Mass = 0.227000 (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 = Body Assembly Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.052167 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.450000 (kg) Final Mass = 0.450000 (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 = Electronics module with batteries Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.017121 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.514000 (kg) Final Mass = 0.514000 (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 = AC7 Propulsion Unit Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.044400 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 0.131000 (kg) Final Mass = 0.131000 (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 = AeroCube7 complete Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 720.000000 (km) Inclination = 98.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.008000 (m^2/kg) Start Year = 2016.000000 (yr) Initial Mass = 2.500000 (kg) Final Mass = 2.500000 (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 =============== 09 11 2015; 09:27:40AM Requirement 4.5-2: Compliant 09 11 2015; 09:27:51AM *********Processing Requirement 4.7-1 Return Status : Passed

***********INPUT**** Item Number = 1 name = Wing Assembly quantity = 2 parent = 0 materialID = 8 type = Box Aero Mass = 0.055000 Thermal Mass = 0.055000 Diameter/Width = 0.079000 Length = 0.150000 Height = 0.025000 name = Wing Assembly quantity = 2 parent = 1 materialID = 8 type = Box Aero Mass = 0.055000 Thermal Mass = 0.055000 Diameter/Width = 0.079000 Length = 0.150000 Height = 0.025000 **************OUTPUT**** Item Number = 1 name = Wing Assembly Demise Altitude = 77.992441 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly Demise Altitude = 0.000000 Debris Casualty Area = 0.947562 Impact Kinetic Energy = 4.371142 ************************************* ***********INPUT**** Item Number = 2 name = Anti-Nadir Lid Assembly quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 0.058300 Thermal Mass = 0.058300 Diameter/Width = 0.103000 Length = 0.108000

Height = 0.002000 name = Anti-Nadir Lid Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.058300 Thermal Mass = 0.058300 Diameter/Width = 0.103000 Length = 0.108000 Height = 0.002000 **************OUTPUT**** Item Number = 2 name = Anti-Nadir Lid Assembly Demise Altitude = 77.987066 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Anti-Nadir Lid Assembly Demise Altitude = 66.743698 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 3 name = Camera Lens (Xenoplan/Schneider) quantity = 1 parent = 0 materialID = 9 type = Cylinder Aero Mass = 0.087200 Thermal Mass = 0.087200 Diameter/Width = 0.032000 name = Camera Lens (Xenoplan/Schneider) quantity = 1 parent = 1 materialID = 9 type = Cylinder Aero Mass = 0.087200 Thermal Mass = 0.087200 Diameter/Width = 0.032000 Length = 0.039000 **************OUTPUT**** Item Number = 3

name = Camera Lens (Xenoplan/Schneider) Demise Altitude = 77.994121 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Camera Lens (Xenoplan/Schneider) Demise Altitude = 72.171480 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 4 name = Rate Gyro Assembly quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 0.095000 Thermal Mass = 0.095000 Diameter/Width = 0.048000 Length = 0.060000 Height = 0.025000 name = Rate Gyro Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.095000 Thermal Mass = 0.095000 Diameter/Width = 0.048000 Length = 0.060000 Height = 0.025000 **************OUTPUT**** Item Number = 4 name = Rate Gyro Assembly Demise Altitude = 77.997980 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Rate Gyro Assembly Demise Altitude = 72.042167 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 *************************************

***********INPUT**** Item Number = 5 name = Nadir Lid Assembly quantity = 1 parent = 0 materialID = 8 type = Flat Plate Aero Mass = 0.187000 Thermal Mass = 0.187000 Diameter/Width = 0.102000 Length = 0.108000 name = Nadir Lid Assembly quantity = 1 parent = 1 materialID = 8 type = Flat Plate Aero Mass = 0.187000 Thermal Mass = 0.187000 Diameter/Width = 0.102000 Length = 0.108000 **************OUTPUT**** Item Number = 5 name = Nadir Lid Assembly Demise Altitude = 77.990199 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly Demise Altitude = 69.956269 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 6 name = Laser Comm Plate quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 0.220700 Thermal Mass = 0.220700 Diameter/Width = 0.102000 Length = 0.103000 Height = 0.019000 name = Laser Comm Plate

quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.220700 Thermal Mass = 0.220700 Diameter/Width = 0.102000 Length = 0.103000 Height = 0.019000 **************OUTPUT**** Item Number = 6 name = Laser Comm Plate Demise Altitude = 77.995691 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Laser Comm Plate Demise Altitude = 69.941308 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 7 name = Laser Isolator quantity = 1 parent = 0 materialID = -1 type = Cylinder Aero Mass = 0.227000 Thermal Mass = 0.227000 Diameter/Width = 0.027000 name = Laser Isolator quantity = 1 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.227000 Thermal Mass = 0.227000 Diameter/Width = 0.027000 Length = 0.072000 **************OUTPUT**** Item Number = 7 name = Laser Isolator Demise Altitude = 77.998035 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Laser Isolator Demise Altitude = 71.501496 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 8 name = Body Assembly quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 0.450000 Thermal Mass = 0.450000 Diameter/Width = 0.113000 Length = 0.160000 Height = 0.106000 name = Body Assembly quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.450000 Thermal Mass = 0.450000 Diameter/Width = 0.113000 Length = 0.160000 Height = 0.106000 **************OUTPUT**** Item Number = 8 name = Body Assembly Demise Altitude = 77.992894 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Assembly Demise Altitude = 71.627253 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 9

name = Electronics module with batteries quantity = 1 parent = 0 materialID = 23 type = Box Aero Mass = 0.514000 Thermal Mass = 0.514000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.070000 name = Electronics module with batteries quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.514000 Thermal Mass = 0.514000 Diameter/Width = 0.080000 Length = 0.080000 Height = 0.070000 **************OUTPUT**** Item Number = 9 name = Electronics module with batteries Demise Altitude = 77.996894 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Electronics module with batteries Demise Altitude = 71.817332 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 10 name = AC7 Propulsion Unit quantity = 1 parent = 0 materialID = 76 type = Box Aero Mass = 0.131000 Thermal Mass = 0.131000 Diameter/Width = 0.057150 Length = 0.088900 Height = 0.044950 name = AC7 Propulsion Unit quantity = 1

parent = 1 materialID = 76 type = Box Aero Mass = 0.131000 Thermal Mass = 0.131000 Diameter/Width = 0.057150 Length = 0.088900 Height = 0.044950 **************OUTPUT**** Item Number = 10 name = AC7 Propulsion Unit Demise Altitude = 77.989488 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = AC7 Propulsion Unit Demise Altitude = 76.931168 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 11 name = AeroCube7 complete quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 2.500000 Thermal Mass = 2.500000 Diameter/Width = 0.100000 Length = 0.150000 Height = 0.100000 name = AeroCube7 complete quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 2.500000 Thermal Mass = 2.500000 Diameter/Width = 0.100000 Length = 0.150000 Height = 0.100000 **************OUTPUT**** Item Number = 11 name = AeroCube7 complete

Demise Altitude = 77.993449 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = AeroCube7 complete Demise Altitude = 65.615120 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============


Document Created: 2015-09-11 21:41:50
Document Modified: 2015-09-11 21:41:50
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