AC8 DAS202 Output v2

0653-EX-PL-2014 Text Documents

Aerospace Corporation, THE

2014-11-03ELS_155332

08 11 2014; 13:40:01PM DAS Application Started 08 11 2014; 13:40:02PM Opened Project C:\Program Files (x86)\NASA\DAS 2.0\IMPACT\ 08 11 2014; 13:40:29PM Processing Requirement 4.3-1: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== 08 11 2014; 13:40:33PM Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== 08 11 2014; 13:40:36PM Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== 08 11 2014; 13:40:42PM Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = AC-8 Space Structure Type = Payload Perigee Altitude = 389.000000 (km) Apogee Altitude = 700.000000 (km) Inclination = 57.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Final Area-To-Mass Ratio = 0.012330 (m^2/kg) Start Year = 2015.100000 (yr) Initial Mass = 2.000000 (kg) Final Mass = 2.000000 (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 =============== 08 11 2014; 13:40:49PM Requirement 4.5-2: Compliant 08 11 2014; 13:40:51PM Processing Requirement 4.6 Return Status : Passed ============== Project Data ============== **INPUT** Space Structure Name = AC-8 Space Structure Type = Payload Perigee Altitude = 389.000000 (km) Apogee Altitude = 700.000000 (km) Inclination = 57.000000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.012330 (m^2/kg) Start Year = 2015.100000 (yr) Initial Mass = 2.000000 (kg) Final Mass = 2.000000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 386.802357 (km) PMD Apogee Altitude = 634.511161 (km) PMD Inclination = 56.996217 (deg) PMD RAAN = 297.816714 (deg) PMD Argument of Perigee = 303.087589 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 386.802357 (km) Suggested Apogee Altitude = 634.511161 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61

Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== 08 11 2014; 13:40:57PM *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AC-8 quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 2.000000 Thermal Mass = 2.000000 Diameter/Width = 0.102500 Length = 0.170000 Height = 0.102500 name = Reaction Wheel Block quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.015000 Thermal Mass = 0.015000 Diameter/Width = 0.028000 Length = 0.029000 Height = 0.028000 name = Antenna-1 quantity = 1 parent = 1 materialID = -3 type = Box Aero Mass = 0.010000 Thermal Mass = 0.010000 Diameter/Width = 0.025000 Length = 0.050000 Height = 0.003000 name = Batteries quantity = 4 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.045000 Thermal Mass = 0.045000 Diameter/Width = 0.018000

Length = 0.065000 name = Torque Rods quantity = 3 parent = 1 materialID = 46 type = Cylinder Aero Mass = 0.005000 Thermal Mass = 0.005000 Diameter/Width = 0.004000 Length = 0.055000 name = Circuit Boards quantity = 1 parent = 1 materialID = -1 type = Box Aero Mass = 0.011970 Thermal Mass = 0.011970 Diameter/Width = 0.056000 Length = 0.056000 Height = 0.002000 name = Lids quantity = 2 parent = 1 materialID = 8 type = Box Aero Mass = 0.086000 Thermal Mass = 0.086000 Diameter/Width = 0.096000 Length = 0.105000 Height = 0.004000 name = Payload Interface Plate quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.120000 Thermal Mass = 0.120000 Diameter/Width = 0.097000 Length = 0.097000 Height = 0.006000 name = VectorNav IMU quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.053000 Thermal Mass = 0.053000

Diameter/Width = 0.042000 Length = 0.048000 Height = 0.025000 name = Bus Electronics Assembly quantity = 1 parent = 1 materialID = -1 type = Box Aero Mass = 0.310000 Thermal Mass = 0.310000 Diameter/Width = 0.078000 Length = 0.089000 Height = 0.055000 name = Payload Assembly quantity = 1 parent = 1 materialID = -1 type = Box Aero Mass = 0.350000 Thermal Mass = 0.350000 Diameter/Width = 0.097000 Length = 0.097000 Height = 0.052000 name = Body Structure quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.595000 Thermal Mass = 0.595000 Diameter/Width = 0.105000 Length = 0.165000 Height = 0.105000 name = Antenna-2 quantity = 1 parent = 1 materialID = -4 type = Box Aero Mass = 0.011000 Thermal Mass = 0.011000 Diameter/Width = 0.044000 Length = 0.046000 Height = 0.003000 **************OUTPUT**** Item Number = 1 name = AC-8

Demise Altitude = 77.994691 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheel Block Demise Altitude = 76.655347 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Antenna-1 Demise Altitude = 76.680785 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Batteries Demise Altitude = 70.235003 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rods Demise Altitude = 75.650340 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Circuit Boards Demise Altitude = 77.971996 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Lids Demise Altitude = 75.858144 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Payload Interface Plate Demise Altitude = 74.891683 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = VectorNav IMU Demise Altitude = 75.283097 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Bus Electronics Assembly Demise Altitude = 77.789488 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Payload Assembly Demise Altitude = 77.789535 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Structure Demise Altitude = 74.010754 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Antenna-2 Demise Altitude = 76.838043 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============


Document Created: 0440-12-05 00:00:00
Document Modified: 0440-12-05 00:00:00
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