AC12 DAS 202 Output No Baffle

0832-EX-CN-2017 Pre Coordination Document

Aerospace Corporation, The

2018-04-04ELS_207531

$04 02 2018; 17:04:27PM DAS Application Started¬ 04 02 2018; 17:04:29PM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC12\New folder\¬ 04 02 2018; 17:04:34PM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC12\New folder\¬ 04 02 2018; 17:04:49PM Mission Editor Changes Applied¬ 04 02 2018; 17:04:53PM Processing Requirement 4.3-1: Return Status : Not Run¬ ¬ =====================¬ No Project Data Available¬ =====================¬ ¬ =============== End of Requirement 4.3-1 ===============¬ 04 02 2018; 17:04:55PM Processing Requirement 4.3-2: Return Status : Passed¬ ¬ =====================¬ No Project Data Available¬ =====================¬ ¬ =============== End of Requirement 4.3-2 ===============¬ 04 02 2018; 17:04:58PM Requirement 4.4-3: Compliant¬ ¬ =============== End of Requirement 4.4-3 ===============¬ 04 02 2018; 17:05:06PM Processing Requirement 4.5-1: Return Status : Passed¬ ¬ ==============¬ Run Data¬ ==============¬ ¬ **INPUT**¬ ¬ Space Structure Name = AC12A¬ Space Structure Type = Payload¬ Perigee Altitude = 450.000000 (km)¬ Apogee Altitude = 450.000000 (km)¬ Inclination = 51.600000 (deg)¬ RAAN = 0.000000 (deg)¬ Argument of Perigee = 0.000000 (deg)¬ Mean Anomaly = 0.000000 (deg)¬ Final Area-To-Mass Ratio = 0.030210 (m^2/kg)¬ Start Year = 2018.000000 (yr)¬ Initial Mass = 4.094000 (kg)¬ Final Mass = 4.094000 (kg)¬ Duration = 1.000000 (yr)¬ Station-Kept = False¬ Abandoned = True¬ PMD Perigee Altitude = -1.000000 (km)¬ PMD Apogee Altitude = -1.000000 (km)¬$

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 ===============¬

04 02 2018; 17:05:10PM Requirement 4.5-2: Compliant¬
04 02 2018; 17:05:11PM 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 = 0.030210 (m^2/kg)¬
Start Year = 2018.000000 (yr)¬
Initial Mass = 4.094000 (kg)¬
Final Mass = 4.094000 (kg)¬
Duration = 1.000000 (yr)¬
Station Kept = False¬
Abandoned = True¬
PMD Perigee Altitude = 420.939331 (km)¬
PMD Apogee Altitude = 436.863640 (km)¬
PMD Inclination = 51.597954 (deg)¬
PMD RAAN = 8.208693 (deg)¬
PMD Argument of Perigee = 124.292371 (deg)¬
PMD Mean Anomaly = 0.000000 (deg)¬
¬
**OUTPUT**¬
¬
Suggested Perigee Altitude = 420.939331 (km)¬
Suggested Apogee Altitude = 436.863640 (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 ===============¬
04 02 2018; 17:05:16PM *********Processing Requirement 4.7-1¬
Return Status : Passed¬
¬
***********INPUT****¬
Item Number = 1 ¬
¬
name = AC12A¬
quantity = 1¬
parent = 0¬
materialID = 8¬
type = Box¬
Aero Mass = 4.094000¬
Thermal Mass = 4.094000¬
Diameter/Width = 0.109000¬

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 = 1.099000¬
Thermal Mass = 0.037000¬
Diameter/Width = 0.082400¬
Length = 0.154500¬
Height = 0.056200¬
¬
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 = 20¬
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 = 20¬
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 = 77.996176¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Nadir Lid Assembly (AC12A)¬
Demise Altitude = 75.501894¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = STIM 210 IMU (AC12A)¬
Demise Altitude = 71.530878¬
Debris Casualty Area = 0.000000¬

Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Optics Holder (AC12A)¬
Demise Altitude = 0.000000¬
Debris Casualty Area = 0.466964¬
Impact Kinetic Energy = 73.202507¬
¬
*************************************¬
name = Optics (AC12A)¬
Demise Altitude = 61.856714¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Front Shim (AC12A)¬
Demise Altitude = 77.664621¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Rear Conical Monolith (AC12A)¬
Demise Altitude = 77.642957¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = O-Ring (AC12A)¬
Demise Altitude = 77.664621¬
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 = 35.609222¬
¬
*************************************¬
name = Imager Base Ring (AC12A)¬
Demise Altitude = 0.000000¬
Debris Casualty Area = 0.392032¬
Impact Kinetic Energy = 19.856871¬
¬
*************************************¬
name = Laser (AC12A)¬
Demise Altitude = 72.169980¬
Debris Casualty Area = 0.000000¬

Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Dosimeter Assembly (AC12A)¬
Demise Altitude = 77.261832¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Dosimeter (AC12A)¬
Demise Altitude = 75.982605¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = PCB (AC12A)¬
Demise Altitude = 76.906777¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Body Base Plate (AC12A0¬
Demise Altitude = 75.940808¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Frame Part 2 (AC12A)¬
Demise Altitude = 76.140277¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Reaction Wheels (AC12A)¬
Demise Altitude = 69.134878¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Reaction Wheels Base (AC12A)¬
Demise Altitude = 76.417449¬
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¬

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 = 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 ===============¬

$04 02 2018; 13:19:05PM DAS Application Started¬ 04 02 2018; 13:19:13PM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC7\DAS2.02 run\¬ 04 02 2018; 13:20:48PM Opened Project C:\Users\jrw29289\Desktop\AeroCubes\AC12\¬ 04 02 2018; 16:18:45PM Processing Requirement 4.3-1: Return Status : Not Run¬ ¬ =====================¬ No Project Data Available¬ =====================¬ ¬ =============== End of Requirement 4.3-1 ===============¬ 04 02 2018; 16:18:48PM Processing Requirement 4.3-2: Return Status : Passed¬ ¬ =====================¬ No Project Data Available¬ =====================¬ ¬ =============== End of Requirement 4.3-2 ===============¬ 04 02 2018; 16:20:42PM Project Data Saved To File¬ 04 02 2018; 16:20:42PM Saved Project As C:\Users\jrw29289\Desktop\AeroCubes\AC12\New folder\¬ 04 02 2018; 16:20:45PM Mission Editor Changes Applied¬ 04 02 2018; 16:20:51PM Processing Requirement 4.3-1: Return Status : Not Run¬ ¬ =====================¬ No Project Data Available¬ =====================¬ ¬ =============== End of Requirement 4.3-1 ===============¬ 04 02 2018; 16:20:53PM Processing Requirement 4.3-2: Return Status : Passed¬ ¬ =====================¬ No Project Data Available¬ =====================¬ ¬ =============== End of Requirement 4.3-2 ===============¬ 04 02 2018; 16:20:56PM Requirement 4.4-3: Compliant¬ ¬ =============== End of Requirement 4.4-3 ===============¬ 04 02 2018; 16:21:01PM Processing Requirement 4.5-1: Return Status : Passed¬ ¬ ==============¬ Run Data¬ ==============¬ ¬ **INPUT**¬ ¬ Space Structure Name = AC12A¬$

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 = 0.030210 (m^2/kg)¬
Start Year = 2018.000000 (yr)¬
Initial Mass = 4.094000 (kg)¬
Final Mass = 4.094000 (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 ===============¬
04 02 2018; 16:21:06PM Requirement 4.5-2: Compliant¬
04 02 2018; 16:21:07PM 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 = 0.030210 (m^2/kg)¬
Start Year = 2018.000000 (yr)¬
Initial Mass = 4.094000 (kg)¬
Final Mass = 4.094000 (kg)¬
Duration = 1.000000 (yr)¬
Station Kept = False¬
Abandoned = True¬
PMD Perigee Altitude = 483.287558 (km)¬
PMD Apogee Altitude = 504.101142 (km)¬
PMD Inclination = 51.599532 (deg)¬
PMD RAAN = 59.947665 (deg)¬
PMD Argument of Perigee = 110.882657 (deg)¬
PMD Mean Anomaly = 0.000000 (deg)¬
¬

**OUTPUT**¬
¬
Suggested Perigee Altitude = 483.287558 (km)¬
Suggested Apogee Altitude = 504.101142 (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 ===============¬
04 02 2018; 16:24:16PM *********Processing Requirement 4.7-1¬
Return Status : Passed¬
¬
***********INPUT****¬
Item Number = 1 ¬
¬
name = AC12A¬
quantity = 1¬
parent = 0¬
materialID = 8¬
type = Box¬
Aero Mass = 4.094000¬
Thermal Mass = 4.094000¬
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¬

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 = 1.099000¬
Thermal Mass = 0.037000¬
Diameter/Width = 0.082400¬
Length = 0.154500¬
Height = 0.056200¬
¬
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 = 20¬
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 = 20¬
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 (AC12A0¬
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 = Zenith Lid Assembly (AC12A)¬
Demise Altitude = 76.441535¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Wing Assembly (AC12A)¬
Demise Altitude = 76.222738¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Telescope Assembly (AC12A)¬
Demise Altitude = 77.664621¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Optics Holder (AC12A)¬
Demise Altitude = 0.000000¬
Debris Casualty Area = 0.466964¬
Impact Kinetic Energy = 73.202507¬
¬
*************************************¬
name = Optics (AC12A)¬
Demise Altitude = 61.856714¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Front Shim (AC12A)¬
Demise Altitude = 77.664621¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Rear Conical Monolith (AC12A)¬
Demise Altitude = 77.642957¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = O-Ring (AC12A)¬
Demise Altitude = 77.664621¬
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 = 35.609222¬
¬
*************************************¬
name = Imager Base Ring (AC12A)¬
Demise Altitude = 0.000000¬
Debris Casualty Area = 0.392032¬
Impact Kinetic Energy = 19.856871¬
¬
*************************************¬
name = Laser (AC12A)¬
Demise Altitude = 72.169980¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Dosimeter Assembly (AC12A)¬
Demise Altitude = 77.261832¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Dosimeter (AC12A)¬
Demise Altitude = 75.982605¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = PCB (AC12A)¬
Demise Altitude = 76.906777¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Body Base Plate (AC12A0¬
Demise Altitude = 75.940808¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Frame Part 2 (AC12A)¬
Demise Altitude = 76.140277¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬

*************************************¬
name = Reaction Wheels (AC12A)¬
Demise Altitude = 69.134878¬
Debris Casualty Area = 0.000000¬
Impact Kinetic Energy = 0.000000¬
¬
*************************************¬
name = Reaction Wheels Base (AC12A)¬
Demise Altitude = 76.417449¬
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¬

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 = 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: 2110-02-15 00:00:00
Document Modified: 2110-02-15 00:00:00