AC7 DAS202 Output v1

0787-EX-PL-2014 Text Documents

Aerospace Corporation, THE

2014-11-07ELS_155495

11 05 2014; 00:32:02AM DAS Application Started
11 05 2014; 00:32:18AM Mission Editor Changes Applied
11 05 2014; 00:32:24AM Processing Requirement 4.3-1:       Return Status:
Passed

==============
Project Data
==============
      Objects Passing Through LEO = True
      Number of Objects = 8

**INPUT**
      Quantity = 1
      Final Area-To-Mass Ratio = 0.009593 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)
      Argument of Perigee = -1.000000 (deg)
      Mean Anomaly = -1.000000 (deg)
      Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 3.485274 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 3.449692 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

**INPUT**
      Quantity = 1
      Final Area-To-Mass Ratio = 0.009732 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)
      Argument of Perigee = -1.000000 (deg)
      Mean Anomaly = -1.000000 (deg)
      Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 3.372260 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 3.367556 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)


     Status = Pass
      Returned Error Message - Normal Processing

==============

**INPUT**
      Quantity = 1
      Final Area-To-Mass Ratio = 0.012231 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)
      Argument of Perigee = -1.000000 (deg)
      Mean Anomaly = -1.000000 (deg)
      Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 2.201027 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 2.176591 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

**INPUT**
      Quantity = 3
      Final Area-To-Mass Ratio = 0.015429 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)
      Argument of Perigee = -1.000000 (deg)
      Mean Anomaly = -1.000000 (deg)
      Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 1.570355 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 4.681725 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

**INPUT**


     Quantity = 4
     Final Area-To-Mass Ratio = 0.014719 (m^2/kg)
     Perigee Altitude = 350.000000 (km)
     Apogee Altitude = 700.000000 (km)
     Inclination = 57.000000 (deg)
     RAAN = -1.000000 (deg)
     Argument of Perigee = -1.000000 (deg)
     Mean Anomaly = -1.000000 (deg)
     Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 1.672814 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 6.570842 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

**INPUT**
      Quantity = 1
      Final Area-To-Mass Ratio = 0.022784 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)
      Argument of Perigee = -1.000000 (deg)
      Mean Anomaly = -1.000000 (deg)
      Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 0.970890 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 0.944559 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

**INPUT**
      Quantity = 2
      Final Area-To-Mass Ratio = 0.023380 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)


     Argument of Perigee = -1.000000 (deg)
     Mean Anomaly = -1.000000 (deg)
     Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 0.940068 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 1.806982 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

**INPUT**
      Quantity = 2
      Final Area-To-Mass Ratio = 0.106413 (m^2/kg)
      Perigee Altitude = 350.000000 (km)
      Apogee Altitude = 700.000000 (km)
      Inclination = 57.000000 (deg)
      RAAN = -1.000000 (deg)
      Argument of Perigee = -1.000000 (deg)
      Mean Anomaly = -1.000000 (deg)
      Released Year = 2015.000000 (yr)

**OUTPUT**
      Perigee Altitude = -6378.136000 (km)
      Apogee Altitude = -6378.136000 (km)
      Inclination = 0.000000 (deg)
      Lifetime = 0.190068 (yr)
      Object Reentered within 25 years of Release = True
      Object-Time = 0.328542 (obj-yrs)
      Total Object-Time = 23.326489 (obj-yrs)
      Status = Pass
       Returned Error Message - Normal Processing

==============

=============== End of Requirement 4.3-1 ===============
11 05 2014; 00:32:26AM Processing Requirement 4.3-2: Return Status:
Passed

=====================
No Project Data Available
=====================

=============== End of Requirement 4.3-2 ===============
11 05 2014; 00:32:28AM Requirement 4.4-3: Compliant

=============== End of Requirement 4.4-3 ===============


11 05 2014; 00:32:29AM Processing Requirement 4.5-1:     Return Status:
Passed

==============
Run Data
==============

=============== End of Requirement 4.5-1 ===============
11 05 2014; 00:32:32AM Requirement 4.5-2: Compliant
11 05 2014; 00:32:32AM Processing Requirement 4.6  Return Status:
Passed

==============
Project Data
==============

=============== End of Requirement 4.6 ===============
11 05 2014; 00:32:36AM *********Processing Requirement 4.7-1
      Return Status: Passed

***********INPUT****
 Item Number = 1

name = Laser Assembly
quantity = 1
parent = 0
materialID = 8
type = Box
Aero Mass = 0.498000
Thermal Mass = 0.498000
Diameter/Width = 0.102000
Length = 0.103000
Height = 0.019000

name = Laser Assembly
quantity = 1
parent = 1
materialID = 8
type = Box
Aero Mass = 0.498000
Thermal Mass = 0.498000
Diameter/Width = 0.102000
Length = 0.103000
Height = 0.019000

**************OUTPUT****
Item Number = 1

name =   Laser Assembly
Demise   Altitude = 77.991605
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************


name =   Laser Assembly
Demise   Altitude = 66.170402
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************

***********INPUT****
 Item Number = 2

name = Body with no wings
quantity = 1
parent = 0
materialID = 8
type = Box
Aero Mass = 1.370000
Thermal Mass = 1.370000
Diameter/Width = 0.100000
Length = 0.150000
Height = 0.100000

name = Body with no wings
quantity = 1
parent = 1
materialID = 8
type = Box
Aero Mass = 1.370000
Thermal Mass = 1.370000
Diameter/Width = 0.100000
Length = 0.150000
Height = 0.100000

**************OUTPUT****
Item Number = 2

name =   Body with no wings
Demise   Altitude = 77.992340
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = Body with no wings
Demise Altitude = 67.719003
Debris Casualty Area = 0.000000
Impact Kinetic Energy = 0.000000

*************************************

***********INPUT****
 Item Number = 3

name = Camera Lens
quantity = 1
parent = 0


materialID = 8
type = Cylinder
Aero Mass = 0.080000
Thermal Mass = 0.080000
Diameter/Width = 0.032000

name = Camera Lens
quantity = 1
parent = 1
materialID = 8
type = Cylinder
Aero Mass = 0.080000
Thermal Mass = 0.080000
Diameter/Width = 0.032000
Length = 0.039000

**************OUTPUT****
Item Number = 3

name =   Camera Lens
Demise   Altitude = 77.998043
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = Camera Lens
Demise Altitude = 71.634433
Debris Casualty Area = 0.000000
Impact Kinetic Energy = 0.000000

*************************************

***********INPUT****
 Item Number = 4

name = Reaction Wheel
quantity = 3
parent = 0
materialID = 54
type = Cylinder
Aero Mass = 0.007000
Thermal Mass = 0.007000
Diameter/Width = 0.012000

name = Reaction Wheel
quantity = 3
parent = 1
materialID = 54
type = Cylinder
Aero Mass = 0.007000
Thermal Mass = 0.007000
Diameter/Width = 0.012000
Length = 0.009000


**************OUTPUT****
Item Number = 4

name =   Reaction Wheel
Demise   Altitude = 77.995512
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = Reaction Wheel
Demise Altitude = 71.743183
Debris Casualty Area = 0.000000
Impact Kinetic Energy = 0.000000

*************************************

***********INPUT****
 Item Number = 5

name = Battery
quantity = 4
parent = 0
materialID = 54
type = Cylinder
Aero Mass = 0.048000
Thermal Mass = 0.048000
Diameter/Width = 0.018000

name = Battery
quantity = 4
parent = 1
materialID = 54
type = Cylinder
Aero Mass = 0.048000
Thermal Mass = 0.048000
Diameter/Width = 0.018000
Length = 0.065000

**************OUTPUT****
Item Number = 5

name =   Battery
Demise   Altitude = 77.998832
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = Battery
Demise Altitude = 65.782480
Debris Casualty Area = 0.000000
Impact Kinetic Energy = 0.000000

*************************************


***********INPUT****
 Item Number = 6

name = STIM
quantity = 1
parent = 0
materialID = 8
type = Box
Aero Mass = 0.052000
Thermal Mass = 0.052000
Diameter/Width = 0.039000
Length = 0.045000
Height = 0.021000

name = STIM
quantity = 1
parent = 1
materialID = 8
type = Box
Aero Mass = 0.052000
Thermal Mass = 0.052000
Diameter/Width = 0.039000
Length = 0.045000
Height = 0.021000

**************OUTPUT****
Item Number = 6

name =   STIM
Demise   Altitude = 77.995722
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = STIM
Demise Altitude = 71.850464
Debris Casualty Area = 0.000000
Impact Kinetic Energy = 0.000000

*************************************

***********INPUT****
 Item Number = 7

name = Lid Assembly
quantity = 2
parent = 0
materialID = 8
type = Box
Aero Mass = 0.187000
Thermal Mass = 0.187000
Diameter/Width = 0.102000
Length = 0.108000
Height = 0.010000


name = Lid Assembly
quantity = 2
parent = 1
materialID = 8
type = Box
Aero Mass = 0.187000
Thermal Mass = 0.187000
Diameter/Width = 0.102000
Length = 0.108000
Height = 0.010000

**************OUTPUT****
Item Number = 7

name =   Lid Assembly
Demise   Altitude = 77.994762
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = Lid Assembly
Demise Altitude = 68.805027
Debris Casualty Area = 0.000000
Impact Kinetic Energy = 0.000000

*************************************

***********INPUT****
 Item Number = 8

name = Wing Assembly
quantity = 2
parent = 0
materialID = 8
type = Box
Aero Mass = 0.055000
Thermal Mass = 0.055000
Diameter/Width = 0.079000
Length = 0.150000
Height = 0.025000

name = Wing Assembly
quantity = 2
parent = 1
materialID = 8
type = Box
Aero Mass = 0.055000
Thermal Mass = 0.055000
Diameter/Width = 0.079000
Length = 0.150000
Height = 0.025000

**************OUTPUT****


Item Number = 8

name =   Wing Assembly
Demise   Altitude = 77.992652
Debris   Casualty Area = 0.000000
Impact   Kinetic Energy = 0.000000

*************************************
name = Wing Assembly
Demise Altitude = 0.000000
Debris Casualty Area = 0.947562
Impact Kinetic Energy = 4.371022

*************************************

=============== End of Requirement 4.7-1 ===============



Document Created: 2014-11-05 00:36:15
Document Modified: 2014-11-05 00:36:15

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