Evaluation of Newly Formulated Dow Corning 321 Dry · PDF fileEvaluation of Newly Formulated...

19
TWR-19912 SHUTTLE Evaluation of Newly Formulated Dow Corning 321 Dry Film Lubricant Final Test Report 29 September 1989 Contract No. NAS8-30490 DR No. 5-3 WBS No. 4B 102-10-06 = - ECS No. SS3432 _='_____1_ CORPORATION SPACE OPERATIONS PO Box 707, Brzgham CHy, UT E4302-0707 (801) B63-3511 Pub_at_ns No. 90197 (NASA-CR-163828) EVALUAT[i]N OF NEWLY FORMULATED DQW CORN[NG 3210RY FILM LUBRICANT Fina| Test Report (fhioko] Corp.) 1_ D CSCL 11C N90-13661 Uncl,_s G3/27 0251581 https://ntrs.nasa.gov/search.jsp?R=19900004345 2018-04-18T01:41:48+00:00Z

Transcript of Evaluation of Newly Formulated Dow Corning 321 Dry · PDF fileEvaluation of Newly Formulated...

Page 1: Evaluation of Newly Formulated Dow Corning 321 Dry · PDF fileEvaluation of Newly Formulated Dow Corning 321 Dry ... Contract No. NAS8-30490 DR No. 5-3 WBS No. 4B 102-10-06 ... Molykote

TWR-19912

SHUTTLE

Evaluation of NewlyFormulated Dow Corning 321

Dry Film Lubricant

Final Test Report

29 September 1989

Contract No. NAS8-30490

DR No. 5-3

WBS No. 4B 102-10-06= - ECS No. SS3432

_='_____1_ CORPORATION

SPACE OPERATIONS

PO Box 707, Brzgham CHy, UT E4302-0707 (801) B63-3511

Pub_at_ns No. 90197

(NASA-CR-163828) EVALUAT[i]N OF NEWLY

FORMULATED DQW CORN[NG 3210RY FILM

LUBRICANT Fina| Test Report (fhioko] Corp.)1_ D CSCL 11C

N90-13661

Uncl,_s

G3/27 0251581

https://ntrs.nasa.gov/search.jsp?R=19900004345 2018-04-18T01:41:48+00:00Z

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_ CORPORATION

SPACE OPERATIONS

TWR-19912

Evaluation of Newly Formulated Dow Corning 321 Dry Film LubricantFinal Test Report

Prepared by:

Test Planning and Reporting

_irements _l_nager

..-._ /: / L,,'/

Program Manager

Approved by:

Fj _Project Engineer

Reliabili_

....PA ,Y._L _- <-_]_ata Management

ECS SS-3432

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ABSTRACT

An evaluationofthe newly formulatedDow Coming 321 dry filmlubricantwas performed on 13

and 14 September 1989 atthe ThiokolEngineeringDevelopment Laboratory,M-53. The purpose

ofthe evaluationwas to compare lubricatingcharacteristicsofDow Corning 321 (STW4-2955,

SCN No. 3) to thoseofMolykote 321R (STW4-2955).

Ten igniterboltswere installedand torquedon testplatesusingthe oldformulationthread

lubricant(Molykote321R),and 10 boltswere installedusingthe new formulation(Dow Coming

321). Afterboltremoval,no signsofgallingwere found on any ofthe boltsor testplatethreaded

holes.Average torque-loadvaluesforeach formulationwere very close.Test resultsshowed there

are no significant differences in lubrication abilities between Molykote 321R and Dow Corning 321.

It is recommended that, once current supplies of Molykote 321R are depleted, Dow Corning

321 dry film lubricant be used in place of Molykote 321R as a thread lubricant on redesigned solid

rocket motor assemblies.

REVISION

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sec I PAse ii

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Section

2

3

4

5

6

7

CONTENTS

Pa e

INTRODUCTION ...................................... 1

1.1 TEST ARTICLE DESCRIPTION ......................... 2

OBJECTIVE ......................................... 4

EXECUTIVE SUMMARY ................................. 5

3.1 SUMMARY ....................................... 5

3.2 CONCLUSIONS .................................... 5

3.3 RECOMMENDATIONS ............................... 5

INSTRUMENTATION ................................... 6

PHOTOGRAPHY ...................................... 6

RESULTS AND DISCUSSION ............................. 7

6.1 ASSEMBLY ....................................... 7

6.2 TEST ........................................... 7

6.3 RESULTS ........................................ 8

APPLICABLE DOCUMENTS .............................. 18

REVISION OOCNO.TWR-19912 I vo,

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_ CORPORAT/ON

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Fibre

1

2

3

4

FIGURES

Pa e

Test Article Assembly ................................... 3

Molykote 321R Torque Test Results ......................... 10

Dow Coming 321 Torque Test Results ........................ 11

Molykote 321R and Dow Coming 321 Torque Test Comparison ....... 12

Tab

1

2

3

TABLES

AerosolDry Film LubricantFormulation ......................

Molykote 321R Torque TestResults .........................

Dow Coming 321 Torque TestResults........................

1

9

9

REVISION

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SECTWR-19912 J vol

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_ CORPORATtON

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1

INTRODUCTION

This reportdocuments the procedures,performance,and resultsobtainedfrom the evaluationof

the newly formulated Dow Corning 321 dry film lubricant. The purpose of the evaluation was to

compare lubricating characteristics of Dow Coming 321 (STW4-2955, SCN No. 3) to those of

Molykote 321R (STW4-2955).

Molykote 321R air drying lubricant spray is currently used as a thread lubricant on valious

redesigned solid rocket motor (RSRM) bolted assemblies including the igniter-to-case joint, case-to-

nozzle joint, and systems tunnel. For safety reasons, supplier Dow Corning Corporation recently

changed the formulation of this lubricant (carcinogens were removed) and also changed the aerosol

can packaging. The old formulation is no longer available. The following is a general descliption

of the changes between old and new formulations:

a. Dow Coming 321 has the same formulation as Molykote 321R except that methylene chloride

solvent (carcinogenic) has been removed and replaced with increased amounts of butyl acetate,

1,1,1-trichloroethane, propane, and butane. The comparative formulations of Molykote 321R

and Dow Coming 321 are shown in Table 1.

b. The new aerosol can provides a more even spray than was provided in previous packaging.

Table 1. AerosolDry Film LubricantFormulation

Dry Film LubricantMolykote 321R Dow Corning 321

Ingredient (percent by weight) (percent by weight)

Nonvolatiles 8 11

Butyl Acetate 2 9

1,1,1-trichloroethane 11 16

Methylene Chloride 44 --

Hydrocarbons 35 64

100 100

REVISION ooc _o. TWR-19912 I VOL

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Testing was therefore necessary to verify that the lubricating characteristics of the new

formulation (Dow Corning 321) do not differ from those of the old formulation (Molykote 321R).

Characteristic differences between the two formulations could affect the torque-load relationship of

the bolts, thus requiring changes to the current torque values. The evaluation did not concern a

specific RSRM assembly; only differences between the two formulations were investigated.

Protection against galling from the new formulation was also evaluated.

The evaluation was performed on 13 and 14 September 1989 at the Thiokol Engineering

Development Laboratory, M-53. The evaluation was performed under CTP-0141, Test Plan to

Evaluate the Newly Formulated Dow Corning 321 Dry Film Lubricant.

1.1 TEST ARTICLE DESCRIPTION

The test article consisted of two test plates and twenty 3/4-in. Inconel 718 igniter bolts (P/N

1U51569-01) as shown in Figure 1. The test plates were machined out of 4340 steel and heat

treated to 180 to 200 ksi to resemble the RSRM case D6AC steel. Eight threaded holes were

machined through the entire thickness of each plate, to allow the bolts to be run through either

side without interference. The threaded holes complied with the threaded bolthole requirements of

the forward case segment (1U51473), refurbished in compliance with the case refurbishment

specification STW7-2744.

REVISION

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sEc [ _oE 2

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SPACE OPERATIONS

'II

IU51569-01 3/4 in,Inconel 718 Igniter Bolt

i !

f_ - ; I

Test Plate -_

Load Collar

Four Strain Gages

I

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. . .., , LI_,_//TyI_A,

IV Jr/Jff/J!

... o , [l,_I/illIA

..:.:.; liiiilil.r,"t " I

illi.... i .................

b ' 8.53 in.8.47 in.

Side View of Test Plate

T2.03 in.1.97 in.

1_

12.28 in.2.22 In.

1.03 in.0.97 in.

.L__

REVISION

50-1,6-UNF-3B

|

1.03t- in.-t,P--

0.97In.

2.19 In.2.13 In.

I

C) G

Top View of Test Plate

Figure 1. Test Article Assembly

oocNO TWR-19912

SEC i PAGE

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2

OBJECTIVE

The objective of test plan CTP-0141 was to evaluate lubricating characteristics of Dow Corning 321

(STW4-2955, SCN No. 3) compared with Molykote 321R (STW4-2955). The evaluation was to

determine if any differences exist in the torque-load relationships between the two formulations.

Also, the evaluation was to verify if galling exists with the use of Dow Coming 321.

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3

EXECUTIVE SUMMARY

3.1 SUMMARY

This section contains an executive summary of the key results from test data evaluation and post-

test inspection. Additional information and details can be found in Section 6, Results and

Discussion.

Ten igniter bolts were installed on the test plates using the old formulation thread lubricant

(Molykote 321R), and 10 bolts were installed using the new formulation (Dow Corning 321). The

bolts were installed, torqued, removed, and inspected one at a time. The bolts were torqued to the

specified load of 55,000 -+5,000 lb in increments of 50 R-lb.

No signs of galling were found on any of the bolts or the test plate threaded holes. Torque-

load data from two bolts coated with Molykote 321R were inconsistent with the majority of the

Molykote 321R data, and were not considered valid data for use in the overall comparison.

Torque-load data from the newly formulated Dow Coming 321 formed a consistent group.

The average of each set of data points at a given bolt loading was plotted, and the averages

of the two formulations were superimposed upon each other (results from two of the Molykote

321R-coated bolts were excluded from the comparison because they were inconsistent with the bulk

of the other results). Average torque-load values for each formulation were very close.

3.2 CONCLUSIONS

Evaluation of the test data supports the conclusion that there are no significant differences in the

lubricating or galling prevention abilities between Molykote 321R and Dow Coming 321.

3.3 RECOMMENDATIONS

It is recommended that, once current supplies of Molykote 321R are depleted, Dow Corning 321

dry film lubricant be used in place of Molykote 321R as a thread lubricant on RSRM assemblies.

.E_s,o. ooc_. TWR-19912 I rot

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_ CORPORAT/ON

SPACE OPERATIONS

4

INSTRUMENTATION

A load collar was used to measure the load at each torque interval. The load collar was

constructed from 4340 steel and heat treated to 190 ksi. The load collar utilized four equally

spaced CEA-06-032UW-120 Micro-Measurements strain gages, mounted every 90 deg. Two of the

gages were mounted 180 deg apart in the axial direction and two were mounted 180 deg apart in

the hoop direction.

The load collar and signal conditioner were operationally verified and electrically zeroed in

accordance with MIL-STD-45662 before and after each bolt evaluation. Initial calibration was

performed with a Baldwin tensile tester.

5

PHOTOGRAPHY

Still color photographs were taken of each bolt and bolthole before installation and after removal of

each bolt. Copies of the photographs (Series No. 112789 and No. 112806) are available from the

Thiokol Photographic Services department.

REVISION

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6

RESULTS AND DISCUSSION

6.1 ASSEMBLY

The two test plates were machined out of 4340 steel and heat treated to 180 to 200 ksi to

resemble the RSRM case D6AC steel (Figure 1). Eight threaded holes were machined through the

entire thickness of each plate. The threaded holes complied with the threaded bolthole

requirements of the forward case segment (1U51473), refurbished in compliance with the case

refurbishment specification STW7-2744.

The test plates, bolts, and boltholes were cleaned with methylchloroform-soaked polywipes

and cotton swabs. Each bolt and at least 20 of the boltholes were inspected, accepted, and

numbered before the evaluation.

The bolt threads were sprayed with one of the two lubricants and allowed to dry for at least

30 sec. A small amount of STW5-2942 (HD-2) grease was applied to the underside of each bolt

head before installation. A load collar was utilized to measure the load at each torque interval

(refer to section 4.0 for additional information about the load collar). Before loading the bolts for

the test, each bolt and threaded hole was exercised three times by torquing the bolt to 50 ft-lb and

then backing out the bolt.

6.2 TEST

Ten ofthe igniterboltswere installedon the testplatesusingthe old formulationthreadlubricant

(Molykote321R),and 10 boltswere installedusingthe new formulation(Dow Coming 321). The

boltswere installed,torqued,removed, and inspectedone at a time.

Boltswith the same lubricantformulationwere not installednext to each other. Each bolt

and threadedholeend was used one time only. For threadedholeswhich had boltstested

through each end,the same lubricantformulationwas used on each bolt.Sixteenboltswere

installedon Block 1 (Holes1 through 16),and fourboltswere installedon Block 2 (Holes25

through 28). The boltswere torquedtothe specifiedloadof55,000 _+5,000Ib in incrementsof50

R-lb. Severalboltswere torquedto loadsslightlylessthan 50,000Ib,becauseitwas predictedthat

they may have failediftheywere tightenedone more 50 ft-lbincrement.

REVISION__ DOCNO. TWR-19912 Jvo,SEC I PAGE 7

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6.3 RESULTS

No signs of galling were found on any of the bolts or the test plate threaded holes.

Axial load values for each bolt were recorded for each torque increment. The results for

Molykote 321R are shown in Table 2 and for Dow Coming 321 in Table 3. Results of Tables 2

and 3 are plotted in Figures 2 and 3, respectively. As shown in Figure 2, torque-load data from

Bolts 6 and 7 were inconsistent with the majority of the Molykote 321R data, and were not

considered valid data for use in the overall comparison. Torque-load data from the newly

formulated Dow Coming 321 formed a consistent group (Figure 3).

The average of each set of data points at a given bolt loading is shown in Figure 4, and the

averages of the two formulations are superimposed upon each other (results from Bolts 6 and 7

were excluded from the comparison because they were inconsistent with the bulk of the other

results). As the plot shows, average values for each formulation at each bolt loading were vezT

close.

.EVlSION__ OOCNo, TWR-19912 I vo,

SEC I _'AaE 890197-1.12

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Table 2. Molykote 321R Torque Test Results(loadin kips)

Torque Bolt Number/Hole Number1_/! 2/3 3/5 4/7 _ s/12 9__ 10/16 6/26 7/28

50 5.265 4.729 4.548 3.464 2.861 4.488 4.187 3.765 2.861 2.861100 10.379 10.331 10.271 8.223 7.680 10.030 9.789 9.548 6.415 6.415150 16.575 18.403 17.017 13.825 14.005 17.800 16.415 16.716 10.030 10.873200 23.253 24.427 20.933 18.704 17.017 24.499 20.752 21.776 11.596 14.427250 27.705 29.848 28.222 25.149 24.306 28.161 27.860 26.716 15.210 18.704300 34.323 39.125 34.306 33.944 33.161 34.366 34.787 32.619 18.885 22.559350 39.437 42.438 39.787 38.402 40.028 40.811400 43.588 47.437 44.124 45.922 47.016 48.341450 49.785 55.931 48.763 50.208 53.220 53.461500 54.056 53.22055O6OO

38.462 39.305 22.258 25.99346.233 44.305 25.571 29.78851.232 49.305 29.968 33.282

53.100 33.824 36.65537.860 42.13740.751 44.847

Table 3. Dow Corning 321 Torque Test Results(loadin kips)

Torque(ft-lb) 11/2 12/4 13/6

Bolt Number/Hole Number15/9 ls/zz 20/15 _ 17/27

50 6.341 5.873 3.946 4.307 3.524 3.464 3.705 4.307 3.765 3.825100 11.943 10.933 9.307 9.849 8.584 7.439 9.729 9.729 8.524 8.343150 17.778 18.343 17.258 17.499 14.427 15.391 18.644 18.523 14.548 15.331200 20.125 24.246 23.824 23.945 18.885 19.427 23.101 21.535 18.644 21.595250 27.465 31.535 32.017 33.462 25.210 25.511 32.077 30.330 23.945 28.342300 31.435 37.920 38.161 41.715 30.390 30.691 39.546 35.992 30.390 35.571350 36.369 43.100 43.040 46.112 35.089 35.089 47.317 43.281 33.643 40.149400 41.783 46.594 48.883 51.473 39.607 42.016 52.919 49.004 38.823 45.148450 46.656 51.895 60.148 44.489 46.654 53.943 43.161 49.184500 53.635 49.907 51.534 49.305 54.786550 52.497

"EVlStON OOCNO TWR-19912 I vo,SEC l PAGE 9

I90197-1.15

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_=___ CORPORATION

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_ CORPORAT/ON

SPA CE OPERA TIONS

7

APPLICABLE DOCUMENTS

Document No.

CTP-0141

STW7-2744

STW5-2942

STW4-2955

MilitaryStandards

MIL-STD-45662

Drawing NO.

1U51473

1U51569

Title

Test Plan to Evaluate the Newly Formulated Dow Coming 321 Dry FilmLubricant

Acceptance Criteria, Refurbished Case, Space Shuttle SRM

Corrosion Preventative Compound and O-ring Lubricant

Lubricant System, Air Drying (Molykote 321R bonded lublicant spray)

Calibration System Requirements

Case Segment, Forward

Bolt, Machine

REVISION

90197-1.13

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_ CORPORATION

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DISTRIBUTION

Recipient

N. BlackD. BurtonS.CardallJ.ChaffeM. CookJ.DainesB. DaveF. DuerschT. Hoffman

R. HyerB. Jurewicz

K. KlingburgG. Larsen

R. LaveryR. MackleyR. McCaskeyB. McQuiveyR. Meyers

R. PapasianK. Peterson

K. SanofskyI_ SperryW. SperryJ. WaltersPrint CribData Management

No. of

111141111111111111451111155

M il top

L71K68243L62L71L61M61851L84L62L70M01242BL71L61L61L72K68E05Lg0851L61L61CE65K23B1L23E

REVISION

90197-1,14

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