AC7 DAS202 Output v2 500 km

0255-EX-CM-2017 Post Grant Documents

Aerospace Corporation, THE

2017-10-26ELS_200333

10 26 2017; 09:32:08AM DAS Application Started 10 26 2017; 09:32:12AM Project Data Saved To File 10 26 2017; 09:32:13AM Opened Project H:\AeroCubes\AC7\Updated Run\DAS2.02 run\ 10 26 2017; 09:32:21AM Mission Editor Changes Applied 10 26 2017; 09:32:26AM Processing Requirement 4.3-1: Return Status : Not Run ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== 10 26 2017; 09:32:28AM Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== 10 26 2017; 09:32:29AM Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== 10 26 2017; 09:32:33AM Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = AeroCube7 complete 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 = 0.004340 (m^2/kg) Start Year = 2017.000000 (yr) Initial Mass = 2.300000 (kg) Final Mass = 2.300000 (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 26 2017; 09:32:34AM Requirement 4.5-2: Compliant 10 26 2017; 09:32:35AM Processing Requirement 4.6 Return Status : Passed ============== Project Data ============== **INPUT** Space Structure Name = AeroCube7 complete 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 = 0.004340 (m^2/kg) Start Year = 2017.000000 (yr) Initial Mass = 2.300000 (kg) Final Mass = 2.300000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 487.478733 (km) PMD Apogee Altitude = 509.921413 (km) PMD Inclination = 51.600284 (deg) PMD RAAN = 62.384617 (deg) PMD Argument of Perigee = 110.818212 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 487.478733 (km) Suggested Apogee Altitude = 509.921413 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2025 (yr) Requirement = 61 Compliance Status = Pass

============== =============== End of Requirement 4.6 =============== 10 26 2017; 09:32:38AM *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AeroCube7 complete quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 2.300000 Thermal Mass = 2.300000 Diameter/Width = 0.100000 Length = 0.150000 Height = 0.100000 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 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 name = Camera Lens (Xenoplan/Schenider) quantity = 1 parent = 1 materialID = 9 type = Cylinder Aero Mass = 0.087200 Thermal Mass = 0.087200 Diameter/Width = 0.032000 Length = 0.039000 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 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 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 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 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 name = Electronis 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 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 = 1 name = AeroCube7 complete Demise Altitude = 77.998699 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly Demise Altitude = 77.252691 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Anti-Nadir Lid Assembly Demise Altitude = 76.719035 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Camera Lens (Xenoplan/Schenider) Demise Altitude = 72.800660 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Rate Gyro Assembly Demise Altitude = 74.621754 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly Demise Altitude = 73.940949

Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Laser Comm Plate Demise Altitude = 73.951222 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Laser Isolator Demise Altitude = 70.805894 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Assembly Demise Altitude = 75.159910 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Electronis Module with Batteries Demise Altitude = 72.955605 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = AC7 Propulsion Unit Demise Altitude = 77.521129 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 =============== 10 26 2017; 09:32:47AM Science and Engineering - Orbit Lifetime/Dwell Time **INPUT** Start Year = 2017.900000 (yr) Perigee Altitude = 500.000000 (km) Apogee Altitude = 500.000000 (km) Inclination = 51.600000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Area-To-Mass Ratio = 0.004340 (m^2/kg) **OUTPUT** Orbital Lifetime from Startyr = 7.452430 (yr) Time Spent in LEO during Lifetime = 7.452430 (yr) Last year of Propagation = 2025 (yr)

Returned Error Message: Object reentered 10 26 2017; 09:32:57AM Project Data Saved To File


Document Created: 2017-10-26 13:53:23
Document Modified: 2017-10-26 13:53:23
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