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The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Page 1: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

The Cost of Maintaining Thermal Protection Systems

Frank E. Jones

NASA-KSC

July 1999

Page 2: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Agenda

Background Design Overview Maintenance Drivers

Factors Affecting Cost Materials Access Touch Time Labor Costs per TPS Type Off Line Support

Improvements To Reduce Cost Presently In-work Future Necessities

Beyond Shuttle

Page 3: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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TPS Surfaces

Lower Surface

Upper Surface

TPS Legend

HRSI (Black) TilesLRSI (White) TilesAFRSI Blankets

GlassExposed Metallic Surfaces

FRSIRCC

Page 4: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Tile Configuration

Densified IML Surface

Silicone RTV Adhesive

SIP

Filler BarCoating Terminator

Uncoated Tile

Koropon-Primed Structure

LRSI Tile White Glass Coating

HRSI Tiles - Black RCG Coating

StepGap

Page 5: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Fibrous Insulation Blankets

RTV Transfer Coated Surface on IML

A

A

Quartz OMLThread

Quartz OML Fabric

D

DC C

View C-C

Section A-A

View B-B

OML FabricFolded Over To IML and Stitched Through Thickness

BB

Quartz Batting

Glass IML Fabric

Glass IML Thread

IML Fabric

OML Thread

Batting

OML Thread

IML Thread

OML Thread

IML Thread

Detail ESection D-DE

OML Fabric

IML fabric

OML Thread

Page 6: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Leading Edge RCC

UpperLeft Wing

Section C-C

CC

Detail D

D

Section E-E

Lower Wing HRSI Tile

Section B-B

Section A-A

B

B

E

Upper Wing AFRSI

Wing Spar

Thermal Barrier

Interface Gap Between RCC and HRSI Tiles

AA

E

Fixed Upstream Gap Between Panel and Tee Seal

Variable Downstream Gap Between Panel and Tee Seal For Thermal Expansion Allowance

I nconel Attachments

ACSS Hardware

RCC Panel (In Foreground)

RCC Tee Seal Web

(In Background)

HRSI Tiles

Upper LESS Access Panel HRSI Tiles

Horsecollar Peripheral Gap Filler Lower LESS Access

Panel HRSI Tile

Upper

Wing

I nconelInsulators

Page 7: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Gap Fillers

Pillow With Sleeving

Pillow Captive Type(Single Lip)

Ames Type

RTV or Ceramic Coated Nextel Fabric

Pillow Captive Type(Double Lip)

Nextel Ceramic Fabric

Saffil Alumina Batting

Inconel Foil

Nextel Ceramic Fabric

Nextel Ceramic Sleeving

Saffil AluminaBatting

Inconel Foil

Pillow or Pad Type

Nextel Ceramic Fabric

Saffil Alumina Batting

Inconel Foil

Saffil Alumina Batting

Inconel Foil

Nextel Sleeving

Nextel Ceramic Fabric

Page 8: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Thermal Barrier & Seal Locations

1 Nose Landing Gear Door

2 FRCS Module/Fuselage Interface

3 Forward RCS Thrusters

4 Crew Hatch

5 Vent Doors

6 Main Landing Gear Doors

7 External Tank Doors

8 Vertical Stabilizer/Fuselage Interface

9 OMS Pod/Fuselage Interface

10 OMS Pod RCS Thrusters

11 Rudder Speed Brake Split Line

Thermal Barriers

A Wing/Elevon

B Aft Fuselage/Body Flap

C Vertical Stabilizer/Rudder Speed Brake

D Payload Bay Door Expansion Joints

E Payload Bay Door Hinge Covers

Aerothermal Seals

Page 9: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Typical Thermal Barrier

RTV-Stiffened Fabric Tail

Inconel Spring Tube

Nextel Sleeving

Nextel Fabric

Thermal Barrier Support

Thermal Barrier Carrier Plate

Main landing Gear Door Side TileThermal Barrier

Structure Side Tile

Typical Thermal Barrier Detail

Main Landing Gear Door Thermal Barrier

Page 10: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Elevon Cove Seal

Lower Elevon TPS

Spanwise Polyimide Primary Seal0.5”

GapHRSI Tiles

Pillow Gap Filler

Lower Wing TPS

Upper Wing TPS FlipperDoor Flipper Door Seal

Elevon Rub Panel

Elevon Rub Tube

Hinge Pins

Uncoated AFRSI Blankets

Page 11: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Orbiter TPS

Average tiles damaged from flight requiring replacement ~20

Average tiles replaced per flow ~75

HRSI tiles on the Orbiter ~19,700 (9 lb), 525 (22 lb)

TUFI tiles on the Orbiter 306 (8 lb)

FRCI tiles on the Orbiter 2,950 (12 lb)

LRSI tiles on the Orbiter 725 (9 lb), 77 (12 lb)

FIB blanket area on the Orbiter 2,123 sq ft

FRSI sheet area on the Orbiter 2,024 sq ft

Page 12: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Flight Damage History

MISSION IMPACTS > 1" TOTAL IMPACTS

STS-41D/FL1 30 111

STS-51A/FLT2 20 87

STS-51C/FLT3 28 81

STS-51D/FLT4 46 152

STS-51G/FLT5 144 315

STS-51I/FLT6 33 141

STS-26R/FLT7 55 411

STS-29R/FLT8 23 132

STS-33R/FLT9 21 118

STS-31R/FLT10 14 63

STS-41/FLT11 16 76

STS-39/FLT12 16 237

STS-48/FLT13 25 182

STS-42/FLT14 44 209

STS-53/FLT15 23 240

STS-56/FLT16 36 156

STS-51/FLT17 18 154

STS-60/FLT18 15 106

STS-64/FLT19 19 150

STS-63/FLT20 14 125

STS-70/FLT21 9 127

STS-82/FLT22 18 103

STS-85/FLT23 6 102

STS-91/FLT24 50 198

STS-95/FLT25 45 187

OV-103 AVERAGE 30.7 158.5

FLEET AVERAGE 31.1 149.2

Page 13: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Materials Cost

Raw Materials* $200k / Flight

Tile PU’s $137k / Flight

Consumables $ 10k / Flight

Total $347k / Flight

* TPSF = RTV’S, Threads, Fabrics, Coatings, etc.

Page 14: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Work Access

Page 15: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Causes for R&R

Flight33.80%

Modification32.39%

Out-of-Tolerance6.34%

Ground Handling5.63%

Access 21.83%

Page 16: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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TPS Discrepancies

RSI Tiles73.75%

FRSI, Filler Bar, and All Others 3.56%

Gap Fillers, Thermal Barriers, and O/T Conditions 16.30%

FI Blankets 3.50%

Re Water Proofing 2.88%

Page 17: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Work Load for Component R&R

Simple NC Tile 35.02%

Complex Splash Tile 7.79%

FRSI 0.20%

Complex NC 25.29%

Simple AFRSI 3.85%

Complex AFRSI 0.72%Tile Reinstallation 4.18%

Simple Splash Tile 22.96%

Page 18: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Labor Hours per Type

0 25 50 75 100

125

150

175

Complex FI Blanket

Simple FI Blanket

FRSI

Reinstall Tile

No Rework NC Tile

Complex NC Tile

Simple NC Tile

Row Time

Touch Labor

Page 19: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Tech Labor Breakdown

Removals & Replacements 55.70%

ML0601-9025 Repairs 12.03%

ML0601 Repairs 10.71%

MDR Repairs 14.27%

ML0601-9024 Rework 4.41%

Re water Proofing 2.88%

Page 20: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Labor Touch Time per TPS Type

• Tile = 2.27 hours/sq.ft.

• FIB = 0.16 hours/sq.ft.

• FRSI = 0.02 hours/sq.ft.

• ET SOFI = 0.70 hours/sq.ft.

Page 21: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Discipline Comparison

Maintenance Technicians 37%

Logistics 3%

Operations 8%Quality Assurance 15%

Engineering 18%

Manufacturing Technicians 19%

Page 22: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Orbiter Processing at KSC

Vehicle Landing Transfer to KSC For Non-KSC Landings

Preparations for Tow

Roll Over To OPF

Orbiter Landing Operations (1 to &+ Days)

Closeout for Right

Rollout To Pad

Orbiter /ET /SRB Mate Test / Checkout in VAB

Rollout to VAB

Pre-Right TestingRewater Proofing

Pre-Rollout InspectionsTPS MaintenancePost Right Inspections

Launch

Launch Pad Operations (3 Weeks)

VAB Operations (1Week)

OPF Operations (10 Weeks)

Page 23: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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OPF Processing

Orbiter Landing at KSC, Tow to OPF, Jack and LevelPLBD Strong back Installation, PLBD Open Up

TPS Post Flight InspectionTPS Waterproofing

TPS Processing

Payload Removal

Payload Bay ReconfigurationFRCS Functional

SSME Heat Shield RemovalSSME Removal

OMS Pod Functional

Hydraulic System Fill and Bleed Removal Aerosurfaces

Fuel Cell Voltage TestPayload Premate Testing

Drag Chute Installation

APU Servicing and CheckoutPayload Bay Cleaning

Payload Installation

SSME InstallationAll Closeouts

Final Payload Bay CleaningET Door Functional

SSME Heat Shield Installation

MPS/ SSME Integration

TPS Rollout Inspection

Landing Gear Door FunctionalPLBD Closure

Orbiter Jack Down, WT & cg, OTV OPSOrbiter Power Down

Roll Out VAB

1 Week

TPS OperationsSSME/MPS Ops

Payload OpsVehicle Ops

Page 24: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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TPS Workforce

0 25 50 75 100 125 150 175

USA Technicians (Incl. 13 Supv.)

USA Quality Assurance (Incl. 2 Supv.)

USA TPS Engineering (Includes Structures)

USA Operations (Incl. Structures and Logistics)

NASA TPS Engineering

NASA Quality Assurance (TPS Dedicated)

NASA Operations and Logistics

BNA TPS Orbiter Engineering

USA TPSF Tecnicians

USA TPSF Quality assurance

USA TPSF Manufacturing Eng.

USA TPSF Support Personnel

BNA TPSF Orbiter Engineering

USA TPSF Logistics

NASA-JSC

USA-JSC / BNA-Houston

BNA-Downey

Pre USA TPSOrganization

Latest TPSOrganization

Page 25: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Past TPS Organization

TPS Organization Personnel

SPC Technicians (Incl. 13 Supv.) 178

SPC Quality Assurance (Incl. 2 Supv.) 47

SPC TPS Engineering 33

SPC Operations 31

NASA TPS Engineering 8

NASA Quality Assurance (TPS Dedicated) 4

NASA Operations and Logistics 3

Rockwell TPS Orbiter Engineering 16

Rockwell TPSF Tecnicians 95

Rockwell TPSF Quality assurance 23

Rockwell TPSF Manufacturing Eng. 5

Rockwell TPSF Support Personnel 6

Rockwell TPSF Orbiter Engineering 4

Rockwell TPSF Logistics 15

NASA-JSC 4

Rockwell-Houston 5

Rockwell-Downey 13

Total TPS Workforce 490

Page 26: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Present TPS Organization

TPS Organization Personnel

USA Technicians (Including 13 Supervisors) 100

USA Quality Assurance (Incl. 2 Supv.) 32

USA TPS Engineering (Includes Structures) 34

USA Operations (Includes Structures and Logistics) 7

NASA TPS Engineering 3

NASA Quality Assurance (TPS Dedicated) 1

NASA Operations and Logistics 1

BNA TPS Orbiter Engineering 10

USA TPSF Tecnicians 52

USA TPSF Quality assurance 11

USA TPSF Manufacturing Eng. 3

USA TPSF Support Personnel 13

BNA TPSF Orbiter Engineering 4

USA TPSF Logistics 5

NASA-JSC 6

USA-JSC 3

BNA-Houston 1

BNA-Downey 32

Total TPS Workforce 318

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Improvements To Reduce Cost

Presently In-work

•Processing Reductions•Less Toxic Re-Waterproofing•Surface Defect Analyzer

Future Improvements

•White TUFI•Ceramic Captive G/F•Thermal Barrier Improvements

Page 28: The Cost of Maintaining Thermal Protection Systems Frank E. Jones NASA-KSC July 1999

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Beyond Shuttle

• Internal Vehicle Health Monitoring

• RF replaces Ground Connections

• No Penetrations

• No Windows

• Self Healing TPS