glast large area telescope: i & t peer review mechanical ground support equipment brian grist

22
GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003 Document: LAT-PR-01779-01 Section 7 - Page 1 GLAST Large Area GLAST Large Area Telescope: Telescope: I & T Peer Review Mechanical Ground Support Equipment Brian Grist SU-SLAC Subsystem Engineer [email protected] 650-926-2998 Gamma-ray Large Gamma-ray Large Area Space Area Space Telescope Telescope

Upload: meena

Post on 18-Mar-2016

52 views

Category:

Documents


1 download

DESCRIPTION

Gamma-ray Large Area Space Telescope. GLAST Large Area Telescope: I & T Peer Review Mechanical Ground Support Equipment Brian Grist SU-SLAC Subsystem Engineer [email protected] 650-926-2998. Outline. MGSE Development Plan Hardware Development List / Rationale Design Factors - PowerPoint PPT Presentation

TRANSCRIPT

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 1

GLAST Large Area Telescope:GLAST Large Area Telescope:I & T Peer Review

Mechanical Ground Support Equipment

Brian GristSU-SLAC

Subsystem Engineer

[email protected]

Gamma-ray Large Gamma-ray Large Area Space Area Space TelescopeTelescope

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 2

OutlineOutline

• MGSE Development Plan– Hardware Development List / Rationale– Design Factors– Proof Testing

• LAT MGSE List– EM-Single Bay Hardware– CU and Flight– Shipping Container Status

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 3

LAT MGSE Development PlanLAT MGSE Development Plan

• LAT-MD-01462, LAT MGSE Development Plan– Summarizes Assembly Sequence, Precedence document is

LAT-PS-00676– Defines MGSE Hardware and Tooling Elements– Defines provision responsibility– All MGSE Designs to Meet EWR 127.1, as Tailored by SLAC

• Material Yield not more than 85% of Ultimate• Design Factor of Safety (No Earth Quake) > 3• Proof Test about 2 times maximum expected load• Earth Quake per SLAC-I-720-0A24E-001, Specification

for Seismic Design at SLAC.– Design for 5% Damping to reduce G loading to 1.5 G at 45º– Does not apply to temporary (crane) operations

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 4

LAT MGSE ListLAT MGSE List1. EM-Cal Rotation / Support Stand (in house)

• Also Used to Rotate EM Single Bay, CU 1 x 4 and then Calorimeter2. EM Lifting Fixture*13. EM ACD Scintillator Support Fixture4. Calorimeter Lift Fixture *2 ( in house) 5. Calorimeter Alignment Tool*2 (in house)

• Includes 0.45 m long Alignment Rods (in house)6. Calibration Unit (1 x 4) to Rotation Stand interface plates (Design Complete)7. CU Integration Stand Proof Test Article (Design Complete)8. Calibration Unit Lift Fixture (in work)9. Calibration Unit ACD Support Fixture10. Calibration Unit X, Y, θ Movement System (for Beam Test)

• 42” Troyke Rotating Table in house ( major find ! )11. Thermal – Dew Point Control Tent (Double Walled) for Beam Test12. CU & LAT Thermal Control Cart Ducting, Hoses, Cold plates13. Grid Perimeter Ring (GPR)

• Supports Grid Through Entire Integration & Test at SLAC• Supports LAT in Shipping Container (To Protect SC Bus Interfaces)

Note: *1 - Tracker Tower Lift Fixture Supplied by Tracker Sub-System

*2 – Successful Installation Demonstration completed Nov. 02

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 5

LAT MGSE ListLAT MGSE List14. Tilt Over Stand

• Two LAT-GPR Support Box Frames tied together by pivot bearing brackets• TBD counterweights to adjust Cg along Z axis during sequential build up • Practice will be required to obtain Tilt Over Certification

15. Special Crane Attachment to GPR (for Tilt Over Operations)• Includes addition of load cell to crane’s lift cable for feedback to operator

during tilt over16. Tilt Over Stand Proof and Protocol Test Article17. ACD Integration Frame18. ACD Lift Fixture19. ACD Lift Fixture Proof Test Article20. LAT Shipping Container

• Insulated for Thermal Cycling Tests• Includes Electrical Feed Throughs to Power up & Receive Data from LAT• Includes Ducting for Thermally Controlled Air Circulation• May Include transits for use of cold plate on X-LAT Heat Plate• Container Cover Lift Fixture (Same as LAT Lift Fixture (TBR))

21. Staging Table (in house)• Preparation / Sub-System Functional Tests

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 6

LAT MGSE ListLAT MGSE List22. Vibration Test Fixture

• Provides Interface Between NRL Vibration Table and LAT to SC Bus Attach Points

• Single Stand Will Support All Three Axes23. Thermal Vacuum Support Kit

• Vibe Test Fixture (VTF) with side support arms for Z axis horizontal• Radiator Support Frame attaches to bottom of VTF and provides lower

attach strut interface• LAT Perimeter Heat Exchanger (to help drive to next temp)

24. Acoustic Test SC Simulator, Very Low Fidelity (TBR)• Open Frame with attach points at – Z end of Radiators

25. Van de Graaff Support Stand (in house)26. Calibration Unit Transport Box

• Includes Dry Air Purge for Humidity Control27. EM Single Bay Transport Box

• For EM transport to Germany (GSI)

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 7

Critical LAT MGSE Integration Steps / Req’tsCritical LAT MGSE Integration Steps / Req’ts

• Grid handling– Grid Perimeter Ring provides attachment points at each of 4 corners;

Consistent with current Radiator Support Structure design– Grid Perimeter Ring includes SC Bus attach bracket interfaces (i.e., all

eight attach points used during shipment; FEA required to validate approach)

• Calorimeter-to-Grid mating– Chosen concept uses alignment tool that interfaces with Calorimeter’s

GSE Support Posts and is lowered into position using Precision Crane• Tracker-to-Grid mating

– 4 attachment points at corners of TKR top plate– Plan to mate Tracker to Grid with alignment tooling (provided by Tracker)

and precision crane operation• ACD-to-Grid mating

– 4 Three Bolt attachment points at corners of BEA, 4 two bolt attachment points mid span on BEA sides

– Plan to mate ACD to Grid using alignment tooling and precision crane operation

– Low Profile Lift Fixture Has Been Added to Hardware List (including needed funding)

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 8

Critical LAT MGSE Integration Steps / Req’tsCritical LAT MGSE Integration Steps / Req’ts

• SLAC Beam Test– De-humidification/cooling system for SLAC Beam Test– Calibration Unit Grid ( 1 X 4), Remote X, Y, Θ Movement System

• True Position Tolerance with respect to Beam is ± 1 mm [0.040”] in X and Y and ± 0.5º in Theta

• SLAC Reference Comprehensive Test / Airborne Cosmic Test (TBR)– De-humidification/cooling/heating system for shipping container– Ship w/o radiators (to fit in aircraft with LAT +Z up)

• NRL Environmental Tests– EMC/EMI – LAT in GPR on Box Stand or LAT on Vibe Test Fixture

on TBD– Random Vibe / Sine Sweep* – Vibe Test Fixture– Acoustic Test – Vibe Test Fixture with Radiator Attach SC

Interface Simulator– Thermal Balance & Cycling in Vacuum – Vibe Test Fixture with SC

Attach Interface Simulator and Side Support Braces

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 9

LAT Transport ContainerLAT Transport Container

• LAT Transport Container– Requires Vibration / Shock Isolation System

• Initial Concept allows 154.2 mm (6”) travel in X, Y and Z for Isolation

• Theoretical Isolation Assessment indicates good loads filtering above 3 Hz

– Baseline Review (July 02) Concept• 2159 mm (85”) Tall by 2921 mm (115”) Wide by 2667 mm

(105”) Deep• Sized with LAT on GPR that attaches to Isolation Frame• Footprint can be reduced if LAT is on VTF, but at the expense

of increased height; Under Evaluation• Fits in the following Aircraft, Upper Cargo Deck Only:

– Boeing 747-100F, 747-200C, Commercial– McDonnel Douglas MD-11, DC-10, Commercial– C130, C141 and C5A, Military Transport

• Will Require a Dedicated (Full Charter) Flight

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 10

LAT Transport Container, Initial ConceptLAT Transport Container, Initial Concept

152.4 mm (6”) Clearance between GPR and inside surface perimeter152.4 mm (6”) Clearance between ACD and TopSide Stiffeners in work

Fits through aircraft doors

2895.6 mm (114”) Across [ 9.5 ft ]

2667 mm (105”) Wide

[ 8.8 ft ] 101.6 mm (4”) x 101.6 mm (4”) x 6.35 mm (1/4”) Wall Box Section

AL

LAT with GPR rests on Shock Isolation Frame

2108.2 mm (83”) Total Height [ 6.9 ft ]

Electrical & Thermal Control feed throughs

in work

Weight Estimate

Container ~ 635 kg (1,400 lbs)

GPR ~ 408 kg (900 lbs)

LAT ~ 2903 kg (6,400 lbs)

Total ~ 3946 kg (8,700 lbs)

~ 513 kg/m2 (105 lbs / ft2)

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 11

LAT MGSE, Van de Graaff on StandLAT MGSE, Van de Graaff on Stand

• Van de Graaff is Ready to Use

Out Riggers for Earthquake Stability Adjustable Feet to Allow Beam

Pipe Height Adjustment

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 12

LAT MGSE, Calorimeter AlignmentLAT MGSE, Calorimeter Alignment

• Alignment Tool and Alignment Rods available and ready to use

Alignment Rods

Handling Fixture Engagement Feature

Handling Fixture Engagement Lever

Jack Screws – Holds Tool Above TEM Connectors

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 13

LAT MGSE, Calorimeter Lift FixtureLAT MGSE, Calorimeter Lift Fixture

• Available, Proof Tested and Ready to UseLift Fixture Turnbuckles Allow

Leveling Adjustment with 10 kg (22 lb) Alignment Tool

Attached

Alignment Tool Weight Reduced to about 4 kg (9.0 lbs)

Calorimeter Mass / Outermost Features

Mock Up ~ 93 kg (205 lbs)

EM-Single Grid Bay

In Modification to Support EM Integration

and Test

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 14

LAT MGSELAT MGSE• EM-Cal Rotation / Support Stand

– Multi-Function, Support EM and CU Integration, Then Acts as Calorimeter Rotation Stand

Calorimeter Rotation Interface

1 x 4 Grid Interface Plate

Also Interfaces with the CU Lift Fixture

1 x 4 Grid, Empty

Level Fine Tune Adjust Tool,

Removed Before Powering Up Drive Motor

(Designed to Fall Away When Person Lets Go of it)

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 15

LAT MGSE CU Integration StandLAT MGSE CU Integration StandProof Test Stand with 1360.8 kg (3,000 lbs)

Install 1st Tracker, Attach Calorimeter to

Rotation Interface with + Z Up

Rotate 1x 4 with Tracker and Calorimeter, Then Attach SLAC Lift Fix Use SLAC Lift Fix and Alignment

System to Install Calorimeter

Calorimeter Alignment System Not Shown for

Clarity

Proof Test Cal Rotation Interface to

204.1 kg (450 lbs)

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 16

LAT MGSE CU Integration StandLAT MGSE CU Integration Stand

EM-Cal Rotation / Support Stand Weldment – In House & Under Assembly

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 17

LAT MGSE, LAT MGSE, Calorimeter Rotation Stand

Calorimeter Interface Assembly

Calorimeter Latches Shown in Lock Down

Position

(Handles Point Inward)

Motor Rotation About 40 Seconds

for 180º

Level Fine Tune Adjust Tool,

Removed Before Powering Up Drive Motor

(Designed to Fall Away When Person Lets Go of it)

Double Worm Gear Reduction Prevents Rotation

When Motor Not Powered

After CU Processing is Complete, 1 x 4 Extension Frame and Driven Side Removed; Calorimeter Rotation Interface Assembly Re-Attached to Become the Calorimeter Rotation Stand

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 18

LAT MGSE, Rotation Concepts / StatusLAT MGSE, Rotation Concepts / Status

• Three concepts under evaluation• Universal Support Stand

– Operationally nice; Provides Up, Down and Rotation– Analytically expensive to manage Seismic Loads

• Tilt Over Stand– See next slide for discussion– Must manage changing Cg along Z during build sequence– Requires personnel access platforms

• Scaled up version of EM-Cal Rotation / Support Stand– Operationally nice, but anticipated to be fairly high off the

ground– Several personnel access platforms would be required

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 19

LAT MGSE, Tilt Over Stand ConceptLAT MGSE, Tilt Over Stand Concept

• Concerns and Mitigations– Tilt Over Shock as LAT passes 90º

• Position GPR along average Cg Z (Study In Work)

• Guide Ropes, Counter Balance Weights, Stop Brackets

– Over Lift of LAT + Stands at High Point• Add load cell to Crane’s Lift Cable to provide

feedback to operator– Available hook height can not support ACD

Installation without special ACD Integration Stand

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 20

LAT MGSE, Tilt Over Stand ConceptLAT MGSE, Tilt Over Stand Concept• Safety Aspects

– All Crane Operations are classified as Hazardous Operations• Due to suspended loads

– Tilt Over Crane Operations are considered Critical Crane Operations

• Critical Crane Operations require more Safety Review Oversight

– Special operator training– Demonstration of correct protocol performance– SLAC Site Certification for the specific tilt over operations with

the specific required equipment» Coordination with SLAC Riggers TBW

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 21

Supplemental Slides

GLAST LAT Project Integration and Test CDR Peer Review, March 28, 2003

Document: LAT-PR-01779-01 Section 7 - Page 22

LAT MGSE Grid Perimeter RingLAT MGSE Grid Perimeter Ring• Depiction of LAT Center of Gravity as a Function of Build Sequence

– From CDR Mass Properties

CMz vs Integration Step

-250.0

-200.0

-150.0

-100.0

-50.0

0.01 4 7 10 13 16 19 22 25 28 31 34 37 40 43 46 49 52 55 58 61 64 67 70 73 76 79

Integration Steps

Z cg

[mm

]Bay

9

Bay8

Bay5

Bay4

Bay10

Bay11

Bay6

Bay7

Bay1

Bay0

Bay3

Bay2

Bay13

Bay12

Bay15

Bay14

ACD

BOXES

Radiators

CMy vs Integration Step

-200.0

-150.0

-100.0

-50.0

0.0

50.0

100.0

1 4 7 10 13 16 19 22 25 28 31 34 37 40 43 46 49 52 55 58 61 64 67 70 73 76 79

Integration Steps

Y c

g [m

m]

Bay9

Bay8

Bay5

Bay4 Bay

10

Bay11

Bay6

Bay7

Bay1

Bay0

Bay3

Bay2

Bay13

Bay12

Bay15

Bay14

ACDBOXES

Radiators

CMx vs Integration Step

-250.0

-200.0

-150.0

-100.0

-50.0

0.0

50.0

1 4 7 10 13 16 19 22 25 28 31 34 37 40 43 46 49 52 55 58 61 64 67 70 73 76 79

Integration Steps

X c

g [m

m]

Bay9

Bay8

Bay5

Bay4

Bay10

Bay11

Bay6 Bay

7

Bay1

Bay0

Bay3Bay

2

Bay13 Bay

12

Bay15Bay

14

ACD

BOXES

Radiators