AC12 DAS 202 Output

0832-EX-CN-2017 Text Documents

Aerospace Corporation, The

2017-10-26ELS_200338

Processing Requirement 4.3-1: Return Status : Not Run ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = AC12A Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 450.000000 (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 = 0.028720 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 4.306000 (kg) Final Mass = 4.306000 (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 = AC12B Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 450.000000 (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 = 0.031096 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 3.977000 (kg) Final Mass = 3.977000 (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 =============== Requirement 4.5-2: Compliant Processing Requirement 4.6 Return Status : Passed ============== Project Data ==============

**INPUT** Space Structure Name = AC12A Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 450.000000 (km) Inclination = 51.600000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg) Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.028720 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 4.306000 (kg) Final Mass = 4.306000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 422.167670 (km) PMD Apogee Altitude = 438.260218 (km) PMD Inclination = 51.598114 (deg) PMD RAAN = 8.775365 (deg) PMD Argument of Perigee = 124.649565 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 422.167670 (km) Suggested Apogee Altitude = 438.260218 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2020 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = AC12B Space Structure Type = Payload Perigee Altitude = 450.000000 (km) Apogee Altitude = 450.000000 (km) Inclination = 51.600000 (deg) RAAN = 0.000000 (deg) Argument of Perigee = 0.000000 (deg)

Mean Anomaly = 0.000000 (deg) Area-To-Mass Ratio = 0.031096 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 3.977000 (kg) Final Mass = 3.977000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 420.189729 (km) PMD Apogee Altitude = 436.014618 (km) PMD Inclination = 51.597856 (deg) PMD RAAN = 7.866433 (deg) PMD Argument of Perigee = 124.073798 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 420.189729 (km) Suggested Apogee Altitude = 436.014618 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2020 (yr) Requirement = 61 Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AC12A quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 4.306000 Thermal Mass = 4.306000 Diameter/Width = 0.109000 Length = 0.340500 Height = 0.103500 name = Nadir Lid Assembly (AC12A) quantity = 1 parent = 1

materialID = 8 type = Box Aero Mass = 0.431000 Thermal Mass = 0.141000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.008000 name = STIM 210 IMU (AC12A) quantity = 1 parent = 2 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 (AC12A) quantity = 4 parent = 2 materialID = 8 type = Box Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.015200 Length = 0.044400 Height = 0.010000 name = Star Tracker (AC12A) quantity = 2 parent = 2 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 (AC12A) 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 = NVIDIA Jetson (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.009000 Thermal Mass = 0.009000 Diameter/Width = 0.050000 Length = 0.087000 Height = 0.014200 name = Torque Rod (AC12A) quantity = 9 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.018000 Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.078700 name = Zenith Lid Assembly (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.084000 Thermal Mass = 0.084000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.016700 name = Wing Assembly (AC12A) 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 = Telescope Assembly (AC12A)

quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 1.311000 Thermal Mass = 0.037000 Diameter/Width = 0.082400 Length = 0.154500 Height = 0.056200 name = Baffle (AC12A) quantity = 1 parent = 11 materialID = 66 type = Cylinder Aero Mass = 0.212000 Thermal Mass = 0.212000 Diameter/Width = 0.051000 Length = 0.093000 name = Optics Holder (AC12A) quantity = 1 parent = 11 materialID = 72 type = Box Aero Mass = 0.243000 Thermal Mass = 0.243000 Diameter/Width = 0.093500 Length = 0.097500 Height = 0.049000 name = Optics (AC12A) quantity = 1 parent = 11 materialID = -2 type = Cylinder Aero Mass = 0.620000 Thermal Mass = 0.620000 Diameter/Width = 0.089500 Length = 0.048600 name = Front Shim (AC12A) quantity = 1 parent = 11 materialID = -3 type = Cylinder Aero Mass = 0.001000 Thermal Mass = 0.001000

Diameter/Width = 0.090500 Length = 0.030000 name = Rear Conical Monolith (AC12A) quantity = 1 parent = 11 materialID = -3 type = Cylinder Aero Mass = 0.006000 Thermal Mass = 0.006000 Diameter/Width = 0.090100 Length = 0.030000 name = O-Ring (AC12A) quantity = 1 parent = 11 materialID = -4 type = Cylinder Aero Mass = 0.005000 Thermal Mass = 0.005000 Diameter/Width = 0.086100 Length = 0.030000 name = Backplate (AC12A) quantity = 1 parent = 11 materialID = 72 type = Cylinder Aero Mass = 0.142000 Thermal Mass = 0.142000 Diameter/Width = 0.101300 Length = 0.040000 name = Imager Base Ring (AC12A) quantity = 1 parent = 11 materialID = 72 type = Cylinder Aero Mass = 0.045000 Thermal Mass = 0.045000 Diameter/Width = 0.045500 Length = 0.015000 name = Laser (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box

Aero Mass = 0.353000 Thermal Mass = 0.353000 Diameter/Width = 0.082200 Length = 0.120700 Height = 0.020200 name = Dosimeter Assembly (AC12A) quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.055000 Thermal Mass = 0.027000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.009500 name = Dosimeter (AC12A) quantity = 2 parent = 21 materialID = 8 type = Box Aero Mass = 0.009000 Thermal Mass = 0.009000 Diameter/Width = 0.025400 Length = 0.035600 Height = 0.004700 name = PCB (AC12A) quantity = 1 parent = 21 materialID = 23 type = Box Aero Mass = 0.010000 Thermal Mass = 0.010000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.001600 name = Body Base Plate (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.262000 Thermal Mass = 0.262000 Diameter/Width = 0.102800 Length = 0.336900

Height = 0.011200 name = Frame Part 2 (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.466000 Thermal Mass = 0.466000 Diameter/Width = 0.102800 Length = 0.336900 Height = 0.097500 name = Reaction Wheels (AC12A) quantity = 3 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.025000 Length = 0.042400 name = Reaction Wheels Base (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.065000 Thermal Mass = 0.065000 Diameter/Width = 0.042800 Length = 0.096800 Height = 0.029200 **************OUTPUT**** Item Number = 1 name = AC12A Demise Altitude = 77.998957 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly (AC12A) Demise Altitude = 75.555090 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = STIM 210 IMU (AC12A) Demise Altitude = 71.643019 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Sensor Block (AC12A) Demise Altitude = 73.800949 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Star Tracker (AC12A) Demise Altitude = 72.372050 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics (AC12A) Demise Altitude = 73.306043 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = NVIDIA Jetson (AC12A) Demise Altitude = 77.713301 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod (AC12A) Demise Altitude = 74.223160 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Assembly (AC12A) Demise Altitude = 76.484394 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly (AC12A) Demise Altitude = 76.269230 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Telescope Assembly (AC12A) Demise Altitude = 77.672808 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Baffle (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.447386 Impact Kinetic Energy = 94.407913 ************************************* name = Optics Holder (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.466964 Impact Kinetic Energy = 73.208908 ************************************* name = Optics (AC12A) Demise Altitude = 62.058890 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Front Shim (AC12A) Demise Altitude = 77.672808 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Rear Conical Monolith (AC12A) Demise Altitude = 77.651496 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = O-Ring (AC12A) Demise Altitude = 77.672808 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Backplate (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.440438 Impact Kinetic Energy = 35.607883

************************************* name = Imager Base Ring (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.392032 Impact Kinetic Energy = 19.855295 ************************************* name = Laser (AC12A) Demise Altitude = 72.280816 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dosimeter Assembly (AC12A) Demise Altitude = 77.283965 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dosimeter (AC12A) Demise Altitude = 76.033855 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = PCB (AC12A) Demise Altitude = 76.934949 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Base Plate (AC12A) Demise Altitude = 75.984847 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Frame Part 2 (AC12A) Demise Altitude = 76.188910 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheels (AC12A) Demise Altitude = 69.285402 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Reaction Wheels Base (AC12A) Demise Altitude = 76.446605 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 2 name = AC12B quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 3.977000 Thermal Mass = 3.977000 Diameter/Width = 0.109000 Length = 0.340500 Height = 0.103500 name = Body Base Plate (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.262000 Thermal Mass = 0.262000 Diameter/Width = 0.102800 Length = 0.336900 Height = 0.011200 name = Frame Part 2 (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.466000 Thermal Mass = 0.466000 Diameter/Width = 0.102800 Length = 0.336900 Height = 0.097500 name = Nadir Lid Assembly (AC12B) quantity = 1 parent = 1 materialID = 8

type = Box Aero Mass = 0.541000 Thermal Mass = 0.141000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.008000 name = STIM 210 IMU (AC12B) quantity = 1 parent = 4 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 (AC12B) quantity = 4 parent = 4 materialID = 8 type = Box Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.015200 Length = 0.044400 Height = 0.010000 name = Star Tracker (AC12B) quantity = 4 parent = 4 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 (AC12B) 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 Wheel Housing (AC12B) quantity = 1 parent = 1 materialID = 54 type = Box Aero Mass = 0.255000 Thermal Mass = 0.010000 Diameter/Width = 0.052800 Length = 0.071100 Height = 0.039200 name = Motor with Reaction Wheel (AC12B) quantity = 3 parent = 9 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.025000 Length = 0.042400 name = Reaction Wheel Base (AC12B) quantity = 1 parent = 9 materialID = 8 type = Box Aero Mass = 0.065000 Thermal Mass = 0.065000 Diameter/Width = 0.042800 Length = 0.096800 Height = 0.029200 name = Torque Rod (AC12B) quantity = 9 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.018000 Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.078700 name = Wing Assembly (AC12B) quantity = 2 parent = 1

materialID = 8 type = Box Aero Mass = 0.148000 Thermal Mass = 0.148000 Diameter/Width = 0.073700 Length = 0.343500 Height = 0.002700 name = Zenith Lid Assembly (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.084000 Thermal Mass = 0.084000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.008000 name = Laser (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.353000 Thermal Mass = 0.353000 Diameter/Width = 0.082200 Length = 0.120700 Height = 0.020200 name = TIM Box (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.100000 Thermal Mass = 0.100000 Diameter/Width = 0.081300 Length = 0.106700 Height = 0.025400 name = Experiment Puck (AC12B) quantity = 9 parent = 1 materialID = 8 type = Box Aero Mass = 0.010000 Thermal Mass = 0.010000

Diameter/Width = 0.024500 Length = 0.024500 Height = 0.024500 name = CNT Epoxy Coupon (AC12B) quantity = 2 parent = 1 materialID = 23 type = Box Aero Mass = 0.030000 Thermal Mass = 0.030000 Diameter/Width = 0.050800 Length = 0.076200 Height = 0.005000 name = Dosimeter Assembly (AC12B) quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.083000 Thermal Mass = 0.055000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.009500 name = Dosimeter (AC12B) quantity = 2 parent = 19 materialID = 8 type = Box Aero Mass = 0.009000 Thermal Mass = 0.009000 Diameter/Width = 0.025400 Length = 0.035600 Height = 0.004700 name = PCB (AC12B) quantity = 1 parent = 19 materialID = 23 type = Box Aero Mass = 0.010000 Thermal Mass = 0.010000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.001600

name = Thruster Bracket (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.047000 Thermal Mass = 0.047000 Diameter/Width = 0.096000 Length = 0.099000 Height = 0.014000 name = Thruster Assembly (AC12B) quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.458000 Thermal Mass = 0.458000 Diameter/Width = 0.096000 Length = 0.096000 Height = 0.062400 name = Thruster Lid (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.044000 Thermal Mass = 0.044000 Diameter/Width = 0.101800 Length = 0.107700 Height = 0.003600 **************OUTPUT**** Item Number = 2 name = AC12B Demise Altitude = 77.998762 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Base Plate (AC12B) Demise Altitude = 75.908871 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 *************************************

name = Frame Part 2 (AC12B) Demise Altitude = 76.125285 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly (AC12B) Demise Altitude = 75.500457 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = STIM 210 IMU (AC12B) Demise Altitude = 71.616886 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Sensor Block (AC12B) Demise Altitude = 73.746996 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Star Tracker (AC12B) Demise Altitude = 72.333542 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics (AC12B) Demise Altitude = 73.158449 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheel Housing (AC12B) Demise Altitude = 75.987683 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Motor with Reaction Wheel (AC12B) Demise Altitude = 67.379191 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 *************************************

name = Reaction Wheel Base (AC12B) Demise Altitude = 74.410089 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod (AC12B) Demise Altitude = 74.070855 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly (AC12B) Demise Altitude = 76.267425 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Assembly (AC12B) Demise Altitude = 76.254230 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Laser (AC12B) Demise Altitude = 72.097308 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = TIM Box (AC12B) Demise Altitude = 76.108972 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Experiment Puck (AC12B) Demise Altitude = 76.895761 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = CNT Epoxy Coupon (AC12B) Demise Altitude = 77.098863 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 *************************************

name = Dosimeter Assembly (AC12B) Demise Altitude = 76.489605 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dosimeter (AC12B) Demise Altitude = 75.202972 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = PCB (AC12B) Demise Altitude = 76.125191 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thruster Bracket (AC12B) Demise Altitude = 76.955855 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thruster Assembly (AC12B) Demise Altitude = 73.760285 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thruster Lid (AC12B) Demise Altitude = 77.002871 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============

=============== 500 KM MISSION ORBIT ANALYSIS =============== Processing Requirement 4.3-1: Return Status : Not Run ===================== No Project Data Available ===================== =============== End of Requirement 4.3-1 =============== Processing Requirement 4.3-2: Return Status : Passed ===================== No Project Data Available ===================== =============== End of Requirement 4.3-2 =============== Requirement 4.4-3: Compliant =============== End of Requirement 4.4-3 =============== Processing Requirement 4.5-1: Return Status : Passed ============== Run Data ============== **INPUT** Space Structure Name = AC12A 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 = 0.028720 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 4.306000 (kg) Final Mass = 4.306000 (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 = AC12B 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 = 0.031096 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 3.977000 (kg) Final Mass = 3.977000 (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 =============== Requirement 4.5-2: Compliant Processing Requirement 4.6 Return Status : Passed ==============

Project Data ============== **INPUT** Space Structure Name = AC12A 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 = 0.028720 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 4.306000 (kg) Final Mass = 4.306000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 483.578629 (km) PMD Apogee Altitude = 504.471831 (km) PMD Inclination = 51.599570 (deg) PMD RAAN = 60.102721 (deg) PMD Argument of Perigee = 110.979079 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 483.578629 (km) Suggested Apogee Altitude = 504.471831 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== **INPUT** Space Structure Name = AC12B 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 = 0.031096 (m^2/kg) Start Year = 2018.000000 (yr) Initial Mass = 3.977000 (kg) Final Mass = 3.977000 (kg) Duration = 1.000000 (yr) Station Kept = False Abandoned = True PMD Perigee Altitude = 483.112913 (km) PMD Apogee Altitude = 503.880160 (km) PMD Inclination = 51.599509 (deg) PMD RAAN = 59.855113 (deg) PMD Argument of Perigee = 110.823841 (deg) PMD Mean Anomaly = 0.000000 (deg) **OUTPUT** Suggested Perigee Altitude = 483.112913 (km) Suggested Apogee Altitude = 503.880160 (km) Returned Error Message = Passes LEO reentry orbit criteria. Released Year = 2021 (yr) Requirement = 61 Compliance Status = Pass ============== =============== End of Requirement 4.6 =============== *********Processing Requirement 4.7-1 Return Status : Passed ***********INPUT**** Item Number = 1 name = AC12A quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 4.306000 Thermal Mass = 4.306000 Diameter/Width = 0.109000 Length = 0.340500 Height = 0.103500 name = Nadir Lid Assembly (AC12A)

quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.431000 Thermal Mass = 0.141000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.008000 name = STIM 210 IMU (AC12A) quantity = 1 parent = 2 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 (AC12A) quantity = 4 parent = 2 materialID = 8 type = Box Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.015200 Length = 0.044400 Height = 0.010000 name = Star Tracker (AC12A) quantity = 2 parent = 2 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 (AC12A) 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 = NVIDIA Jetson (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.009000 Thermal Mass = 0.009000 Diameter/Width = 0.050000 Length = 0.087000 Height = 0.014200 name = Torque Rod (AC12A) quantity = 9 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.018000 Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.078700 name = Zenith Lid Assembly (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.084000 Thermal Mass = 0.084000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.016700 name = Wing Assembly (AC12A) 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 = Telescope Assembly (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 1.311000 Thermal Mass = 0.037000 Diameter/Width = 0.082400 Length = 0.154500 Height = 0.056200 name = Baffle (AC12A) quantity = 1 parent = 11 materialID = 66 type = Cylinder Aero Mass = 0.212000 Thermal Mass = 0.212000 Diameter/Width = 0.051000 Length = 0.093000 name = Optics Holder (AC12A) quantity = 1 parent = 11 materialID = 72 type = Box Aero Mass = 0.243000 Thermal Mass = 0.243000 Diameter/Width = 0.093500 Length = 0.097500 Height = 0.049000 name = Optics (AC12A) quantity = 1 parent = 11 materialID = -2 type = Cylinder Aero Mass = 0.620000 Thermal Mass = 0.620000 Diameter/Width = 0.089500 Length = 0.048600 name = Front Shim (AC12A) quantity = 1 parent = 11 materialID = -3 type = Cylinder

Aero Mass = 0.001000 Thermal Mass = 0.001000 Diameter/Width = 0.090500 Length = 0.030000 name = Rear Conical Monolith (AC12A) quantity = 1 parent = 11 materialID = -3 type = Cylinder Aero Mass = 0.006000 Thermal Mass = 0.006000 Diameter/Width = 0.090100 Length = 0.030000 name = O-Ring (AC12A) quantity = 1 parent = 11 materialID = -4 type = Cylinder Aero Mass = 0.005000 Thermal Mass = 0.005000 Diameter/Width = 0.086100 Length = 0.030000 name = Backplate (AC12A) quantity = 1 parent = 11 materialID = 72 type = Cylinder Aero Mass = 0.142000 Thermal Mass = 0.142000 Diameter/Width = 0.101300 Length = 0.040000 name = Imager Base Ring (AC12A) quantity = 1 parent = 11 materialID = 72 type = Cylinder Aero Mass = 0.045000 Thermal Mass = 0.045000 Diameter/Width = 0.045500 Length = 0.015000 name = Laser (AC12A) quantity = 1 parent = 1

materialID = 8 type = Box Aero Mass = 0.353000 Thermal Mass = 0.353000 Diameter/Width = 0.082200 Length = 0.120700 Height = 0.020200 name = Dosimeter Assembly (AC12A) quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.055000 Thermal Mass = 0.027000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.009500 name = Dosimeter (AC12A) quantity = 2 parent = 21 materialID = 8 type = Box Aero Mass = 0.009000 Thermal Mass = 0.009000 Diameter/Width = 0.025400 Length = 0.035600 Height = 0.004700 name = PCB (AC12A) quantity = 1 parent = 21 materialID = 23 type = Box Aero Mass = 0.010000 Thermal Mass = 0.010000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.001600 name = Body Base Plate (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.262000 Thermal Mass = 0.262000

Diameter/Width = 0.102800 Length = 0.336900 Height = 0.011200 name = Frame Part 2 (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.466000 Thermal Mass = 0.466000 Diameter/Width = 0.102800 Length = 0.336900 Height = 0.097500 name = Reaction Wheels (AC12A) quantity = 3 parent = 1 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.025000 Length = 0.042400 name = Reaction Wheels Base (AC12A) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.065000 Thermal Mass = 0.065000 Diameter/Width = 0.042800 Length = 0.096800 Height = 0.029200 **************OUTPUT**** Item Number = 1 name = AC12A Demise Altitude = 77.998957 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly (AC12A) Demise Altitude = 75.555090 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = STIM 210 IMU (AC12A) Demise Altitude = 71.643019 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Sensor Block (AC12A) Demise Altitude = 73.800949 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Star Tracker (AC12A) Demise Altitude = 72.372050 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics (AC12A) Demise Altitude = 73.306043 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = NVIDIA Jetson (AC12A) Demise Altitude = 77.713301 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod (AC12A) Demise Altitude = 74.223160 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Assembly (AC12A) Demise Altitude = 76.484394 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly (AC12A) Demise Altitude = 76.269230 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Telescope Assembly (AC12A) Demise Altitude = 77.672808 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Baffle (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.447386 Impact Kinetic Energy = 94.407913 ************************************* name = Optics Holder (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.466964 Impact Kinetic Energy = 73.208908 ************************************* name = Optics (AC12A) Demise Altitude = 62.058890 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Front Shim (AC12A) Demise Altitude = 77.672808 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Rear Conical Monolith (AC12A) Demise Altitude = 77.651496 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = O-Ring (AC12A) Demise Altitude = 77.672808 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Backplate (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.440438

Impact Kinetic Energy = 35.607883 ************************************* name = Imager Base Ring (AC12A) Demise Altitude = 0.000000 Debris Casualty Area = 0.392032 Impact Kinetic Energy = 19.855295 ************************************* name = Laser (AC12A) Demise Altitude = 72.280816 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dosimeter Assembly (AC12A) Demise Altitude = 77.283965 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dosimeter (AC12A) Demise Altitude = 76.033855 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = PCB (AC12A) Demise Altitude = 76.934949 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Base Plate (AC12A) Demise Altitude = 75.984847 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Frame Part 2 (AC12A) Demise Altitude = 76.188910 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheels (AC12A) Demise Altitude = 69.285402 Debris Casualty Area = 0.000000

Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheels Base (AC12A) Demise Altitude = 76.446605 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* ***********INPUT**** Item Number = 2 name = AC12B quantity = 1 parent = 0 materialID = 8 type = Box Aero Mass = 3.977000 Thermal Mass = 3.977000 Diameter/Width = 0.109000 Length = 0.340500 Height = 0.103500 name = Body Base Plate (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.262000 Thermal Mass = 0.262000 Diameter/Width = 0.102800 Length = 0.336900 Height = 0.011200 name = Frame Part 2 (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.466000 Thermal Mass = 0.466000 Diameter/Width = 0.102800 Length = 0.336900 Height = 0.097500 name = Nadir Lid Assembly (AC12B) quantity = 1

parent = 1 materialID = 8 type = Box Aero Mass = 0.541000 Thermal Mass = 0.141000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.008000 name = STIM 210 IMU (AC12B) quantity = 1 parent = 4 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 (AC12B) quantity = 4 parent = 4 materialID = 8 type = Box Aero Mass = 0.016000 Thermal Mass = 0.016000 Diameter/Width = 0.015200 Length = 0.044400 Height = 0.010000 name = Star Tracker (AC12B) quantity = 4 parent = 4 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 (AC12B) 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 Wheel Housing (AC12B) quantity = 1 parent = 1 materialID = 54 type = Box Aero Mass = 0.255000 Thermal Mass = 0.010000 Diameter/Width = 0.052800 Length = 0.071100 Height = 0.039200 name = Motor with Reaction Wheel (AC12B) quantity = 3 parent = 9 materialID = 54 type = Cylinder Aero Mass = 0.060000 Thermal Mass = 0.060000 Diameter/Width = 0.025000 Length = 0.042400 name = Reaction Wheel Base (AC12B) quantity = 1 parent = 9 materialID = 8 type = Box Aero Mass = 0.065000 Thermal Mass = 0.065000 Diameter/Width = 0.042800 Length = 0.096800 Height = 0.029200 name = Torque Rod (AC12B) quantity = 9 parent = 1 materialID = -1 type = Cylinder Aero Mass = 0.018000 Thermal Mass = 0.018000 Diameter/Width = 0.008000 Length = 0.078700 name = Wing Assembly (AC12B)

quantity = 2 parent = 1 materialID = 8 type = Box Aero Mass = 0.148000 Thermal Mass = 0.148000 Diameter/Width = 0.073700 Length = 0.343500 Height = 0.002700 name = Zenith Lid Assembly (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.084000 Thermal Mass = 0.084000 Diameter/Width = 0.103500 Length = 0.110900 Height = 0.008000 name = Laser (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.353000 Thermal Mass = 0.353000 Diameter/Width = 0.082200 Length = 0.120700 Height = 0.020200 name = TIM Box (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.100000 Thermal Mass = 0.100000 Diameter/Width = 0.081300 Length = 0.106700 Height = 0.025400 name = Experiment Puck (AC12B) quantity = 9 parent = 1 materialID = 8 type = Box

Aero Mass = 0.010000 Thermal Mass = 0.010000 Diameter/Width = 0.024500 Length = 0.024500 Height = 0.024500 name = CNT Epoxy Coupon (AC12B) quantity = 2 parent = 1 materialID = 23 type = Box Aero Mass = 0.030000 Thermal Mass = 0.030000 Diameter/Width = 0.050800 Length = 0.076200 Height = 0.005000 name = Dosimeter Assembly (AC12B) quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.083000 Thermal Mass = 0.055000 Diameter/Width = 0.052000 Length = 0.071600 Height = 0.009500 name = Dosimeter (AC12B) quantity = 2 parent = 19 materialID = 8 type = Box Aero Mass = 0.009000 Thermal Mass = 0.009000 Diameter/Width = 0.025400 Length = 0.035600 Height = 0.004700 name = PCB (AC12B) quantity = 1 parent = 19 materialID = 23 type = Box Aero Mass = 0.010000 Thermal Mass = 0.010000 Diameter/Width = 0.052000 Length = 0.071600

Height = 0.001600 name = Thruster Bracket (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.047000 Thermal Mass = 0.047000 Diameter/Width = 0.096000 Length = 0.099000 Height = 0.014000 name = Thruster Assembly (AC12B) quantity = 1 parent = 1 materialID = 23 type = Box Aero Mass = 0.458000 Thermal Mass = 0.458000 Diameter/Width = 0.096000 Length = 0.096000 Height = 0.062400 name = Thruster Lid (AC12B) quantity = 1 parent = 1 materialID = 8 type = Box Aero Mass = 0.044000 Thermal Mass = 0.044000 Diameter/Width = 0.101800 Length = 0.107700 Height = 0.003600 **************OUTPUT**** Item Number = 2 name = AC12B Demise Altitude = 77.998762 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Body Base Plate (AC12B) Demise Altitude = 75.908871 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Frame Part 2 (AC12B) Demise Altitude = 76.125285 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Nadir Lid Assembly (AC12B) Demise Altitude = 75.500457 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = STIM 210 IMU (AC12B) Demise Altitude = 71.616886 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Sensor Block (AC12B) Demise Altitude = 73.746996 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Star Tracker (AC12B) Demise Altitude = 72.333542 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Bus Electronics (AC12B) Demise Altitude = 73.158449 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Reaction Wheel Housing (AC12B) Demise Altitude = 75.987683 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Motor with Reaction Wheel (AC12B) Demise Altitude = 67.379191 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Reaction Wheel Base (AC12B) Demise Altitude = 74.410089 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Torque Rod (AC12B) Demise Altitude = 74.070855 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Wing Assembly (AC12B) Demise Altitude = 76.267425 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Zenith Lid Assembly (AC12B) Demise Altitude = 76.254230 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Laser (AC12B) Demise Altitude = 72.097308 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = TIM Box (AC12B) Demise Altitude = 76.108972 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Experiment Puck (AC12B) Demise Altitude = 76.895761 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = CNT Epoxy Coupon (AC12B) Demise Altitude = 77.098863 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000

************************************* name = Dosimeter Assembly (AC12B) Demise Altitude = 76.489605 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Dosimeter (AC12B) Demise Altitude = 75.202972 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = PCB (AC12B) Demise Altitude = 76.125191 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thruster Bracket (AC12B) Demise Altitude = 76.955855 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thruster Assembly (AC12B) Demise Altitude = 73.760285 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* name = Thruster Lid (AC12B) Demise Altitude = 77.002871 Debris Casualty Area = 0.000000 Impact Kinetic Energy = 0.000000 ************************************* =============== End of Requirement 4.7-1 ===============


Document Created: 1950-12-04 00:00:00
Document Modified: 1950-12-04 00:00:00
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