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Test Readiness Review Presenting: Anthony Anglin, Emmett Bailey, Aspen Coates, Zach McConnel, Sierra Williams Other Team Members: Lindsay Goldworm, Elizabeth Luke, Nicholaus Monahan, Mary Scites Customer: Scott Taylor, Surrey Satellite Technology U.S. PAB Advisor: Josh Stamps, Sierra Nevada Corporation Baffling Buffs BAFFLING BUFFS 1

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Page 1: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

TestReadinessReview

Presenting:AnthonyAnglin, EmmettBailey,AspenCoates, ZachMcConnel,SierraWilliams

OtherTeamMembers:LindsayGoldworm,ElizabethLuke,NicholausMonahan,MaryScites

Customer:ScottTaylor,

SurreySatelliteTechnologyU.S.

PABAdvisor:JoshStamps,

SierraNevadaCorporationBaffling

BuffsBAFFLING BUFFS

1

Page 2: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Overview

2

Page 3: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

ProjectMotivation• Startrackersneedtoseedimlightfromdistantstars

• Theycompare whattheyseewithonboardstarcatalogtomakespacecraftattitudeadjustments

• Nearbybodiesemit/reflectstraylightwhichhinders startrackersabilitytoseedimlight

• Bafflesattenuateandeliminatestraylightfromnearbybodies

• Lightweightdeployablebaffleforsmallsats

3Overview Schedule TestReadiness Budget

Page 4: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

ProjectGoals•Developaprototypedeployablebaffleforastartrackertobeusedonasmallsatelliteplatform

•Designandmanufacture adeployablebaffletolimitstraylightintoanopticalsensor

•Developatestmethodologyandinstrumentationsuitetomeasureperformanceofthebaffleforstraylightelimination

•Performthetests forthedeploymentandstraylighteliminationofthebaffle

4Overview Schedule TestReadiness Budget

Page 5: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Requirements&LevelsofSuccessFunctionalRequirements Tier1 Tier2

FR1:Baffleshallbedeployable Manualdeployment Electronicdeploymentwithwiredconnection

FR2:Baffleshallconformtostowedvolumeconstraint

175mmx175mmx50mm 125mmx125mmx50mm

FR3:Baffleshalladheretomassconstraint

<500grams <300grams

FR4:Baffleshallattenuatelightto99.9%

At40° lightincidenceangle At30° lightincidenceangle

5Overview Schedule TestReadiness Budget

Page 6: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Smallsat deployment

Startrackersaturatedbysun

Deploybaffle

Excesslightattenuated

Starpatterndetectedandattitudedetermined

Attitudechanged

ProjectScope

Y

X

Y

X

MissionCONOPS

6Overview Schedule TestReadiness Budget

Page 7: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

DeploymentCONOPS

7

V

Powersenttomotor

PowerScrewRotatesBaffleDeploys

Overview Schedule TestReadiness Budget

Page 8: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationCONOPS

8

0degrees 10to15degrees

Morethan30degrees

Sensor

Overview Schedule TestReadiness Budget

Page 9: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

FunctionalBlockDiagram

9

BaffleDeploymentAssembly

PrecisionMicrodrivesDCMotor

PowerScrew

τMOTOR

3-TieredBaffle

FLIFT

KillSwitchAssembly

BatteryPoweredLaser

Photo-transistor

NPNTransistor

5VtoBase

NarrowLightBeam

3VtoCollector

ExternalComponents

PowerSupply

LabVIEWStation

NIUSB-6009DAQ

3VtoMotor

Windings

LightGenerationandDetection

14-BitDigitalVoltage

30V

HamamatsuPhotodiode

Current-to-VoltageOp-Amp

Light

Light

Photo-current64LED

Source

AnalogVoltage

9

Overview Schedule TestReadiness Budget

Page 10: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

BaselineDesign:CDRvs.Now

LinearBearing

SteelShaft

Vane3Tier3

Vane2Tier2

Vane1Tier1

5/8-20ThreadedRod

PrecisionMicrodrives 212-117

NoMajorStructuralChanges

SinceCDR

Overview Schedule TestReadiness Budget

Sensorwillbehere

10

Page 11: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Schedule

11

Page 12: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

ManufacturingPrep

BraceManufacturing

BaffleManufacturing

BaseplateManufacturing

ManufacturingMargin

Deployment&StrayLightTesting

ResultCompilation

TestingStructureManufacturing

CircuitValidation

- OrderingandDevelopment

- ClassDeliverablePrep

- ClassPresentations&Break

- Manufacturing

- Testing

- CriticalPath

FinalPresentation

FinalsWeek

MSR Today

PCBscreated.Onlyphotodiode&amp.circuitstillneedtobevalidated.Allbraceshavebeencreated.OnschedulesinceMSRMiddletiercomplete,toptier

inprogress,andbottomtiernotstarted.2weeksbehindsinceMSR

1of43Dmoldscreated.Testingstructureinprogress.4daysbehindsinceMSRVaneManufacturing

Vanessentoutofhouseformanufacturing.1weekbehindsinceMSRNotyetmanufactured.1weekbehindsinceMSR

Overall,weare2weeksbehindonmanufacturing.Usingmanufacturingandtestingmargin,theprojectisontime.

12

Page 13: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

TestReadinessOverview

• LightAttenuation&SymmetryTests

• DeploymentTesting

13

Page 14: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

TestReadinessLightAttenuation&SymmetryTests

14

Page 15: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationOverview

• Willbetestinglightattenuationwithrespecttopointingangle

• Twodifferenttests:• Symmetric• Asymmetric

15Overview Schedule TestReadiness Budget 15

SymmetricBaffle

AsymmetricBaffle

Page 16: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

4.9 m

Light Source

Top Down View

LightAttenuationTest

0o

90o

θ

θRotary Table

Overview Schedule TestReadiness Budget

Willvalidatelightattenuation

requirements!

16

Page 17: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

RequirementsToBeValidated

• Lightattenuationtestingwillverifybothoftheserequirements

• Willbetestingbafflesymmetryandasymmetry

Requirement RelativeIncidentPower(P/P0)

Angle(Degrees)

Pass-Band(DR4.3) >95% 10°

Stop-Band(DR4.2) <0.1% 30°

Overview Schedule TestReadiness Budget 17

Page 18: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Final Model

Pre-Obscuration Angle 11.1°

ObscurationAngle 20.7°

Stop

BandRe

quire

men

t

Obscuratio

nAn

gle

PassBandRe

quire

men

t

Pre-Obscuratio

nAn

gle

Overview Schedule TestReadiness Budget

ZemaxValidation– Symmetric ModelExpectedResults

18

Page 19: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

ZemaxValidation– Asymmetric ModelExpectedResults

SteepSide ShallowSide

Pre-Obscuration Angle 8.8° 10.9°ObscurationAngle 19.7° 22.3°

SteepSide

Pre-Obscuratio

n

Stop

BandRe

quire

men

t

PassBandRe

quire

men

t

ShallowSidePre-Obscuratio

n

SteepSide

Obscuratio

n

ShallowSideObscuratio

n

19

Page 20: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

TestReadinessLightAttenuationTestFixtures

20

Page 21: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestFixtures– ExplodedView

21Overview Schedule TestReadiness Budget

Page 22: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestFixtures– ExplodedView

Overview Schedule TestReadiness Budget 22

Alignmentwillbedoneusingcalibrationplate

PVCpipe

CalibrationPlate

Holeemulatingapparentsizeofsun

Baffle

3Dbafflesupport

Baseplate

RotaryTable

Bafflelevelingplate

LightbulbisinsidePVC

140mm

280mm

140mm

Page 23: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

CalibrationMethod– Position

BasePlate

LightStand

Rope268m

m150mm

Overview Schedule TestReadiness Budget 23

Page 24: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

CalibrationMethod– Orientation

95mm 100mm

dd

LightSource

CalibrationPlate

20mm 20mm

20mm

20m

m

145mm

Overview Schedule TestReadiness Budget 24

Page 25: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

CalibrationTestTolerancesPart Tolerance Requirements

Rope(Distance) ±200𝑚𝑚changesFOV by <0.01°

Apparentsundiameter= 0.5°Error:<2%

Laser(Orientation) ±20𝑚𝑚 +ManufacturingError

ChangesResults Angleby0.40°

Pre-obscurationMargin:1.1°

ObscurationMargin:9.3°

Overview Schedule TestReadiness Budget 25

Page 26: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuation&SymmetryTests

EquipmentandNeededFacilities

• CNLcleanroom• Photodiodehandlingitems• LaserSafetyGlasses

Risk

• Delicatephotodioderoutinelycleaned.

• ESDsafeenvironment• Groundallelectronics

26Overview Schedule TestReadiness Budget

Page 27: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestConcernsRisk Mitigation

Alignmentofsensor&lightsource Calibrationplate

Staticelectricity Groundedelectricalcomponents

Eyedamagefromlaserpointers Lasersafetyglassesforcalibration

Photodiodecontamination • Paintmask&powderfreenitrilegloves• Cleanphotodiodewith99%isopropylalcohol

andESDswabs• Cleanbothsidesofthefilter• Handlephotodiodewithplasticantistatic

tweezers• Whennotinuse,storethephotodiodeinan

ESDbagandasecondESDbagwithdesiccant• Willonlyhandlephotodiodeincleanroom

Overview Schedule TestReadiness Budget 27

Page 28: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestProcedure

• TakeP0 measurementat0°• Takepower(P)measurementsevery4°• Between8°-12°,and28°-32°,measurementswillbetakenevery0.1°• CalculatelightattenuationusingrelativepowermeasurementP/P0

Fulltestproceduresavailableuponrequest

28

Page 29: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

TestReadinessDeploymentTesting

29

Page 30: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

DeploymentTestingOverview

• Willbetestingdeploymentwithrespecttotheminimumandmaximumallowabledeploymentheights

30Overview Schedule TestReadiness Budget

Page 31: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

DeploymentTestingOverview• Objective:

• Toensurebafflecantransitionfromastowedtoadeployedstatewithintheexpectedrange

• HowItReducesRisk:• Opticalperformancewillnotbecompromisedifbaffledeployswithinacceptableheight

• AssociatedModel&CircuitValidation:

• Killswitchcircuit(validated)

• KeyData:• Averageheightoffullydeployedbaffle

• Expect: 87mm± 1mm

• Requirement:• FR1:Baffleshallbedeployable

Overview Schedule TestReadiness Budget 31

Page 32: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

DeploymentTesting

87 mm86 mm

2 mm

Bottom of laser pointer at minimum deployment

height!

Laser Pointer Laser

Overview Schedule TestReadiness Budget 32

Page 33: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

DeploymentTestSetUp

Laser Pointer Support

Laser Pointer

Laser Pointer

Laser Pointer Support

Phototransistor

PC Board

“Beam of Light”

“Beam of Light”

PCB Support

PCB Support

Overview Schedule TestReadiness Budget 33

Page 34: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

DeploymentTestProcedure• Ensurebottomoflaserpointerisatacceptableminimumdeploymentheight

• Turnonlaserpointertostartdeployment• Whenfullydeployed,laserlighttophototransistorwillbeimpededcausingvoltagetomotortostopendingdeployment

• Repeatformaximumacceptabledeploymentheight

• Location:• Bobby’sLab

34Overview Schedule TestReadiness Budget

Page 35: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

TestingStatusTest Status: Awaiting:LightAttenuationTest(Symmetrical)

Notcompleted • 13Dbafflenegative• Baffle• Baseplate

LightAttenuationTest(Asymmetrical)

Notcompleted • 23Dbafflenegatives• Baffle• Baseplate

DeploymentTest Notcompleted • Baffle• Baseplate• Laserpointersupport• PCB• PCBsupport

35Overview Schedule TestReadiness Budget

Page 36: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Budget

36

Page 37: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Electronics, $52.93TestingEquipment,

$835.82

Optics, $1,006.94

StockMetal, $258.80

BaffleAdd-Ons,$269.32

Safety/Handling,$50.76

Other, $748.95

FutureCostsEstimate,$600.00

Margin, $1,176.48

BUDGET

37

Electronics - $52.93Testing Equipment - $835.82Optics - $1,006.94Stock Metal - $258.80Baffle Add-Ons - $269.32Safety/Handling - $50.76Other - $748.95Future Costs Estimate - $600.00

Sum - $3,823.52

Margin - $1,176.48

Page 38: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

References

38

Page 39: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

References• http://cnl.colorado.edu/cnl/index.php?option=com_content&view=article&id=211&Itemid=155

• http://www.cleanairtechnology.com/cleanroom-classifications-class.php

• https://static.rapidonline.com/catalogueimages/Module/M071087P01WL.jpg

39

Page 40: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

BackupSlides

40

Page 41: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

BackupSlides• Zemax

• FinalModelSpecs• AsymmetricModelSpecs• ParallelRayModel

• Specs• Results

• MeshRefinementStudy• Specs• Results• Analysis

• 4PhotodiodesSpecs

• BaffleNegativeCAD

41

Page 42: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Breakdown

42

•Electronics•Includes PC board, resistors, batteries and other small components

•Testing Equipment•Includes lasers, light bulbs, diffuser disk, and test setup material

•Optics•Includes filter, primary photodiode, and backup photodiodes

•Stock Metal•Includes Aluminum 2024-T4

•Baffle Add-Ons•Includes thread tap, bearing, shaft, motor, and gear

•Safety/Handling•Includes alcohol cleaner, ESD safe tweezers, gloves, dust mask, and static control bag

•Other•Includes epoxy, adhesive, printing, Aeroglaze coating and shipping costs

•Future Costs Estimate•Vanes ($150), Coating application ($200), Felt ($250)

Page 43: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

FinancialSummary

43

• All items (except 1) are currently in the locker•Felt for the light attenuation test needs to be purchased

•Future cost include:•Re-ordering items/stock material if necessary•Outsourcing vanes

•$150•Will get back this week

•Application of coating on baffle•2-3 days

Page 44: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTest- CalibrationPlate

Overview Schedule TestReadiness Budget 44

Page 45: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestFixtures- ExplodedView

Overview Schedule TestReadiness Budget 45

Page 46: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestFixtures

Overview Schedule TestReadiness Budget 46

Page 47: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

LightAttenuationTestFixtures

Overview Schedule TestReadiness Budget 47

Page 48: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

2nd Tiershift–PrimaryDegreeofFreedom

2nd Tiershifts

‘Steepside’‘ShallowSide’

δ

θθ - δ

• ‘ShallowSide’s’effectiveFOVremainsthesame.

• ‘SteepSide’s’newfieldofviewis‘designed’–‘perturbedangle’

Overview Schedule TestReadiness Budget 48

Page 49: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

- OrderingandDevelopment

- ClassDeliverablePrep

- ClassPresentations&Break

- Manufacturing

- Testing

- CriticalPath49

Page 50: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Specification– FinalModel

• BaffleModel:Fullydeployedwithvanesandcoating

• Resolution:0.1°• AngleSweep:(0° to30°)• Numberofraysfromlightsource:

• 200,000,000rays

50

Tier3

Tier2

Tier1

Page 51: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Specification- AsymmetricTest

• BaffleModel:Maximummiddletieroffsetfullydeployedwithvanesandcoating

• Resolution:0.1°• AngleSweep:(0° to30°)• Numberofraysfromlightsource:

• 10,000,000rays

51

2mm

Page 52: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Specifications– ParallelRays

• BaffleModel:Symmetricfullydeployedwithvanesandcoating

• Resolution:0.1°• AngleSweep:(0° to12.4°)• Distance:15m• Numberofraysfromlightsource:

• 200,000,000rays

52

Distance=15000mm

Page 53: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Results– ParallelRays

53

15m 4.88m

Pre-Obscuration Angle 11.4° 11.1°

ObscurationAngle N/A 20.7°

15m 4.88m

AngleFromParallel 0.19° 0.58°

Pre-ObscurationAngleZone

PassBandRe

quire

men

t

Page 54: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Specifications- MeshIndependence

• BaffleModel:Symmetricfullydeployedwithvanesandcoating

• Resolution:0.1°• AngleSweep:(0° to30°)• Distance:4.88m• Numberofraysfromlightsource:

• 10,000,000rays• 100,000,000rays• 200,000,000rays

54

49m

m

StrayLightRays

44mm

30.25mm

18mm

Page 55: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Results-MeshIndependence

55

Pre-ObscurationAngleZone

ObscurationAngleZone

Page 56: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Analysis-MeshIndependence

56

10,000,000Rays 100,000,000Rays

Pre-Obscuration Error 3.6% 1.8%

ObscurationError 1.9% 0

𝑃𝑒𝑟𝑐𝑒𝑛𝑡𝐸𝑟𝑟𝑜𝑟 = 𝐸𝑥𝑝𝑒𝑟𝑖𝑚𝑒𝑛𝑡𝑎𝑙 − 𝑇𝑟𝑢𝑡ℎ

𝑇𝑟𝑢𝑡ℎx100

Requirement 10,000,000Rays 100,000,000Rays 200,000,000Rays(Truth)

Pre-Obscuration >10° 11.5° 10.9° 11.1°

Obscuration <30° 21.1° 20.7° 20.7°

Page 57: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

Specification– 4Photodiodes

• BaffleModel:Maximummiddletieroffsetfullydeployedwithvanesandcoating

• Resolution:0.1°• AngleSweep:(0° to30°)• NumberofDetectors:4• Numberofraysfromlightsource:

• 10,000,000rays

• NotCompletedasof(03/06/17)

57

1.4m

m10

mm

10mm

13.2mm

9mm

11.4mm

Page 58: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDA– horizontalorientation,symmetricallineup(metricunits)

58

87.154

250.000

116.508

39.334

63.989

15.000

66.000

21.403

12.000

12.000

20.000

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS:MM

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 59: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDA– horizontalorientation,symmetricallineup(Englishunits)

59

3.431

9.843

4.587

1.549

2.519

.591

2.598

.843

.472

.472

.787

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS:INCHES

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 60: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDB– horizontalorientation,asymmetricallineup(metricunits)

60

14.732

87.250

250.170

116.341

63.994

39.990

67.869

11.036

12.968

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS: MM

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 61: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDB– horizontalorientation,symmetricallineup(Englishunits)

61

.580

3.435

9.849

4.580

2.519

1.574

2.672

.434

.511

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS: INCHES

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 62: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDC– verticalorientation,symmetricallineup(metricunits)

62

87.949 63.929 39.887

80.000

87.250

250.059

87.949

63.929

14.732

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS: MM

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 63: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDC– verticalorientation,symmetricallineup(Englishunits)

63

3.463 2.517 1.570

3.150

3.435

9.845

3.463

2.517

.580

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS: INCHES

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 64: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDD– verticalorientation,asymmetricallineup(metricunits)

64

250.554

87.250

88.000

63.974

14.309

11.987

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS:MM

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 65: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

MOLDC– verticalorientation,asymmetricallineup(Englishunits)

65

9.864

3.435

3.465

2.519

.563

.472

REV. DESCRIPTION DATE

TOLERANCESUNLESSNOTED:

UNITS: INCHES

PROPRIETARY AND CONFIDENTIAL

THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF UNIVERSITY OF COLORADO. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT WRITTEN PERMISSION IS PROHIBITED.

SHEET

1 of 1REVPN

DESCRIPTION

UNIVERSITY OF COLORADO

1111 ENGINEERING DRIVEBOULDER, CO 80309-0427

FINISH

MATERIAL

X.X 0.050 X.XX 0.010 X.XXX 0.005 X.X 1

Page 66: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

ElectronicCircuits– BreadboardTestingMotorDeploymentCircuit/KillSwitch

• STATUS: Verifiedviabreadboardtest

• PLAN: OrderPCBandsoldercomponents

• COMPLETION: March14

• ADDITIONALINFO: Phototransistorisonlysensitivetohighintensitygreenlight(530nm)

• Darkroomnotrequiredfordeploymenttesting• Personnelsafetyhazardsreducedduetowelllittestingarea

66

Page 67: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

ElectronicCircuits– BreadboardTestingSensorandAmplifierCircuit

• STATUS: Breadboardtestinginprogress(March6)

• PLAN: Completetesting,orderPCB,andsoldercomponents

• COMPLETION: March14

• ADDITIONALINFO: Breadboardtestingdelayedduetotheneedforcleanroomcontrolsforsafehandlingofcomponent

• ColoradoNanofabricationLaboratorygrantedfreeaccess• Photodiodesolderingwillalsobeperformedatthissite• Lightattenuationtestingwillalsobeperformedatthissite

67

Page 68: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

CleanroomControls

• GrantedfreeaccesstoColoradoNanofabricationLaboratorycleanroomfacility• Typically$58/hour

• Class1000cleanroom– Fewerparticlesthannormalambientairbyafactorof1000• CleanerthanaClass10,000cleanroom

• ConsiderednecessaryforsafehandlingofHamamatsuphotodiode

• Additionalequipmentrequired• Bluecoatandbooties

• NightaccessgrantedtofacilitatecleanLightAttenuationtesting• Eliminatesneedtohermeticallysealthefilter/photodiodeassemblyonthebafflebaseplate

68

Page 69: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

SensorandAmplifierCircuit– NoiseReduction

• Twisted,shieldedwirepairforphotodiodeleads• Groundshieldtoreducenoise

• FaradayCage– Metalenclosureforcircuit• GroundedviaGNDpinonDAQtoreducenoise• SalvagedfromElectronicsLab

PCB

DAQCPU

FaradayCage

TwistedWirePairUSB

GroundedShield

GroundedFaradayCageviaDAQUSBtoCPUground 69

Page 70: Test Readiness Review - University of Colorado Boulder · 2017-10-04 · Project Goals •Develop a prototype deployable baffle for a star tracker to be used on a small satellite

OrientationVerificationLightSource

LaserBeam

10mm20m

m𝜃C4900mm

20mm

𝜃C = tanGH204900

𝜃C = 0.23°

𝜃 = 𝜃C +𝜃K𝜃 = 0.23° + 0.17°𝜃 = 0.40°

𝜃K88.25mm

0.254mm

𝜃K = tanGH0.25488.25

𝜃K = 0.17°

21mm

20mm

Overview Schedule TestReadiness Budget 70