AP2

Validation of Alternatives to Aliphatic Isocyanate

Polyurethanes

Presented by : Joseph Curran

NASA Corrosion Technology LabsKennedy Space Center, FL

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National Aeronautics and Space Administration (NASA) Headquarters chartered the Acquisition Pollution Prevention (AP2) Office to coordinate agency activities affecting pollution prevention issues identified during system and component acquisition and sustainment processes.

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The primary objectives of the AP2 Office are:

Reduce or eliminate the use of hazardous materials (HazMats) or hazardous processes at manufacturing, remanufacturing, and sustainment locations.

Avoid duplication of effort in actions required to reduce or eliminate HazMats through joint center cooperation and technology sharing.

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NASA Corrosion Technology Laboratories through the USTDC contract at Kennedy Space Center is tasked to perform the necessary screening, laboratory, and field tests for this project as outlined in the Joint Test Protocol.

KSC Beach Atmospheric Corrosion Test Site

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FACILITIES-CAPABILITIES:

Atmospheric exposure siteElectrochemistry labSeawater immersion systemCoatings application labAccelerated corrosion equipmentWebsite (http://corrosion.ksc.nasa.gov)

NASA Corrosion Technology LaboratoryMISSION: To develop corrosion control and detection technologies. To investigate, evaluate, & determine material behavior in corrosive environments To reduce the use of hazardous materials

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Outline Why replace aliphatic isocyanate polyurethanes? Overview of validation procedures Test Coupon Matrix Coating Selection Results of Tests Conclusion Future Studies Acknowledgements

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Why replace aliphatic isocyanate polyurethanes?Isocyanates are classified as potential human carcinogens and are known to cause cancer in animals.The Occupational Health & Safety Administration (OSHA) states that the effects of isocyanate exposure include:

irritation of skin and mucous membranes chest tightness difficult breathing

Effects of overexposure: occupational asthma lung problems irritation of the eyes, nose, throat, and skin.

AP2 Overview of Validation Procedures

This JTP was created from engineering, performance, and operational impact requirements defined by a consensus of NASA and Air Force Space Command (AFSPC) participants and contains the requirements and tests necessary to qualify coating alternatives for Aliphatic Isocyanate Polyurethane applications.

AP2 Overview of Validation ProceduresPhase One Screening Tests

TEST REFERENCE

Pot Life (Viscosity) ASTM D1200

Ease of Application ASTM E376

Surface Appearance ASTM D523, D2244

Accelerated Storage Stability ASTM D1849

Cure Time ASTM D4752

Cleanability MIL-PRF-8328D, -85285

X-Cut Adhesion ASTM D3359

Tensile Adhesion ASTM D4541

Knife Test FED-STD-141

AP2 Overview of Validation ProceduresPhase Two Laboratory Tests

TEST REFERENCE

Removability ASTM D1200Repairability ASTM E376Abrasion Resistance ASTM D523, D2244Gravelometer ASTM D1849Fungus Resistance N/AAccelerated Weathering ASTM D4752Filiform Resistance MIL-PRF-8328D, -85285Mandrel Bend Flexibility ASTM D3359Marine Exposure Environment ASTM D4541Cyclic Corrosion Resistance FED-STD-141Hypergol Compatibility KSC MTB-175-88, NASA-STD-6001LOX Compatibility NASA-STD-6001

AP2 Overview of Validation ProceduresField Evaluations

(To be performed at Stennis Space Center, MS)

TEST REFERENCEEase of Application Technician EvaluationSurface Appearance ASTM E523, D2244Dry-To-Touch Technician Evaluation

Rocket motor test stand to be used for test coating application

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Test Coupon Matrix per SystemSize Quantity Type Alloy

4"x6"x .1875" 24 Composite A-36 steel4"x6"x .1875" 45 Flat A-36 steel3"x6"x .1875" 6* Flat A-36 steel4"x12"x.1875" 6 Flat A-36 steel4"x4"x .032" 6 Flat 1008 steel3"x5"x .032" 12 Flat 1008 steel3"x5"x .025" 6 Flat 3003 H14Aluminum**.75" round 60 Flat Disc 304 Stainless Steel4"x4" 15 Flat Aluminum Foil

*40 for the control coating/ **one system only

AP2 Coating Selections

Manufacturer ProductCoating

Type System UseCarbozinc 11HS (primer) Carboguard 893 (intermediate) Carboxane 2000 (top)

IO ZincEpoxy

Siloxane

IO ZincEpoxy

Urethane

IO ZincSiloxaneIO ZincAcrylicIO ZincAcrylic

1 Test

Carbozinc 11HS (primer) Carboguard 893 (intermediate) Carbothane 134 HB (top)

2 Control

Zinc Clad 11 WB (primer) Polysiloxane XLE (top) 3 Test

Zinc Clad 11 WB (primer) Fast Clad HB (top) 4 Test

Zinc Clad 11 WB (primer) Sher-Cryl HPA (top) 5 Test

Carboline

Sherwin Williams

AP2 Coating Selections Cont.

Manufacturer ProductCoating

TypeSyste

m UseInterzinc 22 (primer) Interseal 670 HS (intermediate) Interfine 979 (top)

IO ZincEpoxy

SiloxaneIO ZincEpoxy

SiloxaneIO ZincEpoxy

UrethaneUrethaneUrethaneUrethaneIO ZincEpoxy

Siloxane

6 TestInterzinc 22 (primer) Interseal 670 HS (intermediate) Interfine 878 (top) 7 Test

ICI Devoe Coatings

Cathacote 304V (primer) Devron 201 (intermediate) Devathane 359 (top) 8 Control

AquaSurTech Coating Products

D45-20 (primer) WB D45-AMS (top) WB D45-AMS (clear coat) WB 9 Test

Ameron International

Dimecoat 9H (primer) Amercoat 383 (intermediate) PSX-1001 (top) 10

International Protective Coatings

Test

AP2 Test ResultsPot Life

Pot life was determined using a procedure to determine the viscosity increase of a mixed multi-component liquid coating system at room temperature and heated (solvent-borne only) over a specified time. Viscosity was measured, using Zahn Cups, initially and at 30 minute intervals for a period of 4 hours or until failure. Cup efflux times in seconds (T) was convertedto viscosity values (V) in centistokes (cks) using the followingequations* for each respective cup:

Cup 1: V= 1.59T (1070 T)Cup 2: Not UsedCup 3: V= 10.23T (575 T)Cup 4: V= 15.13T (545 T)Cup 5: V= 27.27T (540 T)

*Equations derived from NIST traceable standard viscous oils.

AP2 Test ResultsPot Life

cup time (sec)

viscosity (cks)

cup time (sec)

viscosity (cks)

1 5 48 1298 57 1545 4 hrs yes2* 4 32 475 115 1743 1.5 hrs no3 4 56 845 31 459 4 hrs yes456 4 30 428 66 990 4 hrs yes7 3 35 336 48 484 4 hrs yes8* 5 35 911 60 1627 2 hrs no910 3 28 260 14 102 4 hrs yes

Water-BasedWater-Based

Water-Based

SystemZahn Cup

Initial 25oC Final 35oCTime

Interval Sprayable

Viscosity of Heated Samples 35OC

* control coatings

AP2 Test Results

Viscosity of Room Temperature Samples 25OC

cup time (sec)

viscosity (cks)

cup time (sec)

viscosity (cks)

1 5 48 1298 79 2161 4 hrs no2* 4 32 475 108 1637 2.5 hrs no3 4 56 845 50 746 4 hrs yes4 4 60 899 76 1143 4 hrs yes5 4 46 684 56 838 4 hrs yes6 4 30 428 93 1394 4 hrs yes7 3 35 336 67 672 4 hrs yes8* 5 35 911 52 1394 4 hrs yes9 1 73 101 77 109 4 hrs yes

10 3 28 260 28 102 4 hrs yes

SprayableZahn CupSystem

Initial 25oC Final 25oCTime

Interval

* control coatings

Pot Life

AP2 Test Results

Application Criteria EvaluationSystem Wet Coat Finish Runs Bubbles Sags Hiding

1 Smooth Gloss >7 wet no >7 wet 1 coat2 Smooth Gloss no no no 2 coat*3 Smooth Gloss no yes** no 1 coat4 Smooth Gloss no yes** no 1 coat5 Smooth Gloss no yes** no 1 coat6 Smooth Gloss no no no 1 coat7 Smooth Gloss no no no 1 coat8 Smooth Gloss no no no 1 coat9 Smooth Semi-gloss >1 wet no >1 wet 2 coat*

10 Smooth Gloss no no no 1 coat*thin film coating/ **due to spraying directly on zinc primer

AP2 Test Results

Visual Surface AppearanceCoating System Unaided Eye

1 Smooth glossy finish with uniform color.2 Slight orange peel, glossy finish with uniform color.3 Smooth glossy finish with uniform color.4 Smooth semi-gloss appearance with uniform color.5 Smooth semi-gloss appearance with uniform color.6 Slight orange peel, glossy finish with uniform color.7 Slight orange peel, glossy finish with uniform color.8 Smooth glossy finish with uniform color.9 Smooth semi-gloss appearance with uniform color.

10 Smooth glossy finish with uniform color.

AP2 Test Results

Visual Surface AppearanceCoating System 10x Magnification

1 No defects or irregularities observed.2 No defects or irregularities observed.3 No defects or irregularities observed.4 Small crater-like anomalies observed on surface.5 Small crater-like anomalies observed on surface.6 No defects or irregularities observed.7 No defects or irregularities observed.8 No defects or irregularities observed.9 No defects or irregularities observed.10 No defects or irregularities observed.

AP2 Test Results

This test evaluates any changes in consistency and certain other properties that may take place when liquid coatings are stored at a temperature above 32F. This test simulates some of the effects of storage for 6 months to 1 year at 75 3.5F. One quart samples were obtained from each coating system. Each un-opened container was evaluated for any skinning, corrosion on the interior of the can, odors of putrefaction, rancidity, or souring. The samples were weighed and stored, undisturbed for one-month at 125 2F, and re-evaluated. Then the coatings were applied to test coupons by brush and the finish was examined for grains, lumps, and/or streaks.

ASTM D1849 Standard Test Method for Package Stability of Paint

AP2 Test Results

ASTM D1849-95 Container Conditionand Coating Finish Ratings

10 None8 Very Slight6 Slight4 Moderate2 Considerable0 Complete Failure

AP2 Test Results

ASTM D1849-95 Pre- and Post Oven ContainerCondition Results

Pre Post Pre Post Pre Post Pre Post Pre Post1 1503.2 1501.8 10 10 10 10 10 10 10 42 1180.8 1180.8 10 8 10 10 10 10 10 43 1161.3 1161.3 10 10 10 8 10 10 10 104 1000.2 999.4 10 10 10 10 10 10 10 105 1199.5 1198.9 10 8 10 10 10 10 10 106 1207.7 1207.5 10 8 10 10 10 10 10 27 1217.8 1217.8 10 8 10 8 10 10 10 48 1185.8 1185.1 10 8 10 10 10 10 10 89 1162.3 1162.0 10 6 10 10 10 10 10 1010 1110.2 1109.8 10 10 10 6 10 10 10 10

Corrosion OdorCoating System

Weight Skinning Pressure

AP2 Test Results

ASTM D1849-95 Post-OvenBrushed Coating Finish Results

Grains Lumps Streaks1 10 10 102 10 10 103 10 10 104 10 10 105 10 10 106 10 10 107 8 8 108 10 10 109 10 10 1010 10 10 10

Coating System

Coating Appearance

AP2 Test ResultsCure Time Test

ASTM D4752 Resistance RatingsThis practice describes a solvent rub technique for

assessing the cure of an organic coating.

Rating Remarks

5 No effect on surface; no coating on cloth.

4 Burnished appearance in rubbed area; slight amount of coating on cloth.

3 Some marring and apparent depression of the film.

2 Heavy marring; obvious depression in the film.

1 Heavy depression in the film but no penetration to the primer.

0 Penetration to the primer.

AP2 Test ResultsASTM D4752 Solvent Rub Ratings

ASTM RatingSystem Acetone MEK

1 5 5 2 02* 5 5 4 03 5 5 2 04 1 0 14 2.3 mils5 1 1 14 2.5 mils6 5 5 2 07 5 5 2 08* 5 5 2 09 5 5 2 010 0 0 14 2.9 mils

# of days

Film Loss

* control coating systems

AP2 Test Results

System 4 Solvent Rub Test Photographs

(0) (0) (0)

(0) (0) (0)

(2) (0) (1)

(0) (0) (0)

(ratings)

AP2 Test Results

System 5 Solvent Rub Test Photographs (ratings)

(1) (1) (2)

(0) (1) (1)

(2) (2) (1)

(1) (1) (1)

AP2 Test Results

System 10 Solvent Rub Test Photographs(ratings)

(0) (0) (0)

(0) (0) (0)

(0) (0) (0)

(0) (0) (0)

AP2 Test ResultsCleanability

This test evaluates the resistance of a topcoat to soil adhesion and staining. Performed using MIL-PRF-85285 (Coating: Polyurethane, Aircraft and Support Equipment, issued 1988, revised 2002) section 4.6.13 as a guideline.

Cleaning Efficiency = [(C-B) / (A-B)] 100%.

Where:A= initial L* valueB= soiled sample L* valueC= final cleaned L* value

AP2 Test ResultsCleanabilityTest Results

Coating System Cleaning Efficiency (%)1 972* 973 974 375 76 997 988* 989 9610 15

*control coatings

AP2 Test ResultsCleanability

SYS 1 SYS 2* SYS 3 SYS 4 SYS 5

SYS 6 SYS 7 SYS 8* SYS 9 SYS 10

*control coatings

AP2 Test Results

Wet X-Cut Tape Adhesion

X-cut adhesion test were performed in accordance with FED-STD-141 Method 6301.3, Adhesion (Wet) Tape Test, and evaluated using ASTM D 3359, Standard Test Methods for Measuring Adhesion by Tape Test, approved 1995, revised 2002), Method A. Panels were immersed in DI water for 24 hours, dried with a cloth, and scribed with an X. Tape was applied on the scribe and removed.

AP2 Test Results

Wet X-Cut Tape Adhesion

ASTM D3359-02 Scribe Ratings5A4A3A2A1A0A

Removal from most of the area of the X under the tape.Removal beyond the area of the X.

No peeling or removal.Trace peeling or removal along incisions or at their intersection.Jagged removal along incisions up to 1.6 mm (1/16") on either side.Jagged removal along most incisions up to 3.2 mm (1/8") on either side.

AP2 Test Results

Wet X-Cut Adhesion Tape Test Results

Coating System

ASTM Rating

1 3A2 5A3 2A4 0A5 4A6 3A7 5A8 4A9 5A10 0A

Scribe tool caused jagged edges along incisionScribe tool caused jagged edges along incision

No damageCoating was removed between parrallel lines

Coating was severly blistered and was removedTrace peeling along incision

Scribe tool caused jagged edges along incision

Failure Mode

Scribe tool caused jagged edges along incisionNo damage

Scribe tool caused jagged edges along incision

AP2 Test Results

Wet X-Cut Adhesion Tape Test Results

Sys 1 Sys 2* Sys 3 Sys 4 Sys 5

Sys 6 Sys 7 Sys 8* Sys 9 Sys 10

*control coatings

AP2 Test Results

ASTM D4541 Tensile Adhesion

ASTM D4541 test evaluates the pull-off adhesion strength of a coating. The test determines either the greatest perpendicular force (in tension) that a surface area can bear before a plug of material is detached. Failures are described as percentages of adhesion or cohesion of coating system interfaces.

AP2 Test Results

Dolly

Glue

Top Coat

Mid Coat

PrimerSubstrate

3-Coat System

2-Coat System

Coating System Interfaces

AP2 Test Results

ASTM D4541 Pull-Off Adhesion Results

Primer Mid-Coat Top-Coat Glue1 1765 10%C 90%A2 2100 85%C 10%A 2%A 3%A3 2050 n/a 100%A4 935 n/a 100%A5 760 n/a 100%C6 1830 100%C7 1785 99%C 1%A8 2180 40%C 50%C 10%A9 2235 100%A10 855 100%A

A- adhesion failure C - cohesion failure

Coating System

Tensile Adhesion

(psi)

Failure Interface

AP2 Test ResultsDolly Pull-Off Adhesion Photographs

SYS 1 SYS 2* SYS 3 SYS 4 SYS 5

SYS 6 SYS 7 SYS 8* SYS 9 SYS 10

*control coatings

AP2 Test Results

Knife Test

The purpose of this test is to evaluate the various coatings for brittleness, toughness, and tendency to ribbon by cutting narrow parallel lines in the coating with a serviceable knife that has a sharp blade. The test was performed in accordance with FED-STD-141, Paint, Varnish, Lacquer and RelatedMaterials: Methods of Inspection, Sampling and Testing, approved 2001, Method 6304.2.

AP2 Test Results

FED STD 141D Knife Test Results

Coating System

12345678910

Coating Condition

Some chipping on scribed lines/ no peelingNo chipping or peeling

Slight chipping/ no peeling

No chipping or peelingNo chipping or peeling

Several lines disbonded and peeled

No chipping/ Slight peelingNo chipping or peelingNo chipping or peelingNo chipping or peeling

AP2 Test Results

FED STD 141D Knife Test Photographs

SYS 1 SYS 2* SYS 3 SYS 4 SYS 5

SYS 6 SYS 7 SYS 8* SYS 9 SYS 10

*control coatings

AP2 Test ResultsSummary

Coating SystemsTest 1 2 3 4 5 6 7 8 9 10

Pot Life (Heated) B C B B B B B C B BPot Life (Room Temp) W C S S S S S C S SEase of Application S C S S S S S C W SSurface Appearance S C S S S S S C S SAccelerated Storage S C S B S S W C S SCure Time S C S W W S S C S WCleanability S C S W W S S C S WX-Cut Adhesion W C W W S W S C S WTensile Adhesion W C W W W S S C B WKnife Test W C S S S S S C S W

C- Control B- Better S- Similar W- Worse

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Conclusion

After review of the Phase One screening tests, coating systems 1,4,5, and 10 are being considered for elimination from the Phase Two testing.

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Future Studies Abrasion Filiform Mandrel bend Chip resistance Fungus resistance Accelerated weathering Removability and Repair tests Marine exposure Cyclic Corrosion Resistance Hypergol Compatibility LOX Compatibility

AP2

Thank youFor more information contact:

NASA AP2 Office:

Kevin Andrews 321-867-8477

Pattie Lewis 321-867-9163http://www.acqp2.nasa.gov/

NASA Corrosion Technology Laboratories:

Jerry Curran 321-867-9486http://corrosion.ksc.nasa.gov/