RFQ_80NSSC19Q0781.pdf

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Attached to: Flight Fittings
Solicitation number: 80NSSC19Q0781
Issued by: National Aeronautics and Space Administration Shared Services Center

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1 V2.0 9-22

National Aeronautics and Space Administration

NASA Shared Services Center Stennis Space Center, MS 39529-6000

6/24/2019

SUBJECT: Request for Quotation (RFQ) 80NSSC19Q0781, Flight Fittings

This solicitation includes the following sections:

1. Statement of Work/Bid Schedule – Section 1

2. Instructions to Offerors – Section 2

3. Solicitation Provisions/Representations and Certifications – Section 3

4. Clauses/Terms and Conditions – Section 4

5. Quote Evaluation Criteria – Section 5

SECTION 1

STATEMENT OF WORK/BID SCHEDULE

This a Brand Name or Equal To requirement.

Effective Date: 06/18/2019 Expiration Date: 06/18/2024

Check https://ipdtdms.gsfc.nasa.gov to verify that this is the correct version prior to use

400-FORM-0002 (4/16/2014)

EUROPA-PROP-SOW-0036, Revision B EUROPA Clipper Propulsion, Code 597

Flight Fittings Statement of Work

Goddard Space Flight Center Greenbelt, Maryland

National Aeronautics and

Space Administration

GSFC EUROPA Clipper Propulsion CMO K. Mrowczynski

06/18/2019

RELEASED

https://ipdtdms.gsfc.nasa.gov/

Flight Fittings Statement of Work EUROPA-PROP-SOW-0027, Revision B i

Flight Fittings Statement of Work

Signature/Approval Page

Prepared by:

Melissa Harris

Reviewers/Approvers:

Caitlin Bacha David Benson Matthew Fox

Approved by:

Caitlin Bacha

*** Electronic signatures are available on-line at: https://ipdtdms.gsfc.nasa.gov*** https://ipdtdms.gsfc.nasa.gov/

Flight Fittings Statement of Work EUROPA-PROP-SOW-0036, Revision B ii

Preface

This document is a Europa Clipper Propulsion signature-controlled document. Changes to this document require prior approval of the applicable Product Design Lead (PDL) or designee. Proposed changes shall be submitted in the Technical Data Management System (TDMS) via a Signature Control Request (SCoRe) along with supportive material justifying the proposed change. Changes to this document will be made by complete revision.

All of the requirements in this document assume the use of the word "shall" unless otherwise stated.

Questions or comments concerning this document should be addressed to:

Europa Configuration Management Office Mail Stop: 597 Goddard Space Flight Center Greenbelt, Maryland 20771 iii

Change History Log

Revision Effective Date Description of Changes (Reference the SCoRe Approval Date)

Revision A

06/06/2019 Released following the approval of EUROPA-ScoRe-

Revision B 06/11/2019 Fixed a typo in the drawings. Removed 2278642 and added 2278641.

Revision B 06/18/2019 Released following approval of EUROPA-ScoRe-0379 iv

Contents 1 Introduction

1.1 General Information

1.2 Scope

1.3 SOW Compliance

1.4 Applicable Documents

2 Hardware

2.1 Specifications of fittings

3 Documentation 4 Delivery 5 Proposal Options ..................................................... Error! Bookmark not defined.

Flight Fittings Statement of Work EUROPA-PROP-SOW-0027, Revision B

1 INTRODUCTION

1.1 GENERAL INFORMATION

The Europa Clipper (EC) mission is being formulated and implemented by a joint partnership between the Jet Propulsion Laboratory (JPL) and the Applied Physics Laboratory (APL), with NASA Goddard Space Flight Center (GSFC) building the propulsion system for the APL.

This Statement of Work (SOW) details the characteristics, quantities, and delivery of titanium flight fittings for the EC Propulsion Subsystem.

1.2 SCOPE

The supplier shall provide the facilities, personnel, services, tools, equipment, and materials necessary to manufacture and deliver hardware in accordance with the requirements of this SOW and the documents referenced herein.

1.3 SOW COMPLIANCE

The supplier shall note any section in this SOW that cannot be met or has partial compliance.

The format of the SOW compliance may be a matrix listing each section in this statement of work reflecting a non-compliance. Areas of non-compliance may be cooperatively addressed with GSFC.

1.4 APPLICABLE DOCUMENTS

All applicable and reference documentation identified in this document shall apply in the situations where they are specifically referenced.

2 HARDWARE

2.1 SPECIFICATIONS OF FITTINGS

The supplier shall follow the specifications listed and shown in the drawings provided by GSFC.

Table 1 includes the list of drawing numbers provided by GSFC with their respective descriptions and quantities. The supplier shall manufacture according to the quantities listed in Table 1. The material of the fittings shall be titanium 6AL-4V BAR, annealed condition, in accordance with SAE-AMS-4928W “Titanium Alloy Bars, Forging, Rings, and Drawn Shapes, 6AL-4V, Annealed”.

Table 1: GSFC drawing number, drawing title and quantity required.

3 DOCUMENTATION

The supplier shall supply material certificate of conformance, including source information, lot number, heat number, dimensional inspection certification and relevant test results (i.e.

acceptance tests and periodic tests) for every fitting.

The supplier shall deliver the documentation described in this section as hard copies that are delivered with the fittings and/or in electronic form sent via electronic means.

4 DELIVERY

The supplier shall ship the fittings specified in the previous sections, visually clean and individually bagged in resealable packages, Free on Board (F.O.B). The supplier shall deliver the fittings per the schedule provided with the quote and agreed to by NASA. The supplier shall be liable for any damage incurred during shipment.

GSFC Drawing # Description Quantity Required

2278626 ELBOW, 1/4", HIGH PRESSURE 6

2278627 ELBOW, 1/4", LOW PRESSURE 13

2278630

ELBOW, HIGH PRESSURE, 1/4” PCA PURGE

VALVE 4

2278638 ELBOW, REDUCING, 3/8" TO 1/4” 4

2278640 TRIBOW, REDUCING, 3/8" TO 1/4" 4

2278641 TRIBOW, 1/4" 4

2278643 ELBOW, 1/4", LONG LEG 4

F O L D

L I N E

F O L D

L I N E

REV 03/2019

DWG. NO.

REVISION

DESCRIPTION ZONEREV

INC EO 1-A

THIRD ANGLE PROJECTION

INCH

XHYBRID

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE: CREO 3.0

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

0.01

.XXX

0.001

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

R.010 OR CHAMFER MAX.

�a� µIN

METRIC BLOCK TOLERANCE: MM

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

R0.25 OR CHAMFER MAX.

µM

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

FITTING, ELBOW,

1/4", HIGH PRESSURE

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278626

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278626 FITTING, ELBOW, 1/4" HP TITANIUM, 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED.

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIMUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

This document contains information within the purview of the Export Administration Regulations (EAR), 15 CFR §730-774, and is export-controlled. It may not be transferred to foreign nationals in the U.S. or abroad without specific approval of a knowledgeable export control official, and/or unless an export license or license exception is obtained/available from the Bureau of Industry and Security, United States Department of Commerce.

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REV 08/2016

16,669 0,254 .656 .010[ ]

7,938 0,254 .313 .010[ ]

6,35 +0,102

.250 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

7,938 0,254 .313 .010[ ]

A�|�B

SR 2,286 0,051

.090 .002[ ]

2X 0,89 0,102 .035 .004[ ]

2X R0,254 +0,254

.010 +.010 -.000[ ]

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

FITTING, ELBOW,

1/4", HIGH PRESSURE

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278626

REV

SCALE: 4/1 SHEET: 2 OF 2

SECTION A-A

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE: CREO 3.0

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

.01

.XXX

.001

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

ELBOW, HIGH PRESSURE,

1/4", PCA PURGE VALVE

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278630

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278630 ELBOW, 1/4" HP TI 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED".

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIMUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

L D

L I N E

F O L D

L I N E

REV 08/2016

29,369 0,254

1.156 .010[ ]

13,969 0,254 .550 .010[ ]

7,938 0,254 .313 .010[ ]

6,35 +0,102

.250 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

7,938 0,254 .313 .010[ ]

SR 2,286 0,051

.090 .002[ ]

2X 0,89 0,102 .035 .004[ ]

2X R0,254 +0,254

.010 +.010

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

ELBOW, HIGH PRESSURE,

1/4", PCA PURGE VALVE

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278630

REV

SCALE: 4/1 SHEET: 2 OF 2

SECTION A-A

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REVISION

DESCRIPTION ZONEREV

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE: CREO 3.0

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

.02

.XXX

.005

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

METRIC BLOCK TOLERANCE: MM

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

TRIBOW, REDUCING,

3/8" TO 1/4"

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278640

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278640 TRIBOW, REDICING, 3/8" TO 1/4" TI 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED".

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIMUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

L D

L I N E

F O L D

L I N E

REV 08/2016

18,263 0,254 .719 .010[ ]

3X 0,71 0,102 .028 .004[ ]

11,125 0,254 .438 .010[ ]

9,525 +0,102

.375 +.004 -.000[ ]

9,525 +0,102

.375 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

11,125 0,254 .438 .010[ ]

SR 4,051 0,051

.159 .002[ ]

3X R0,254 +0,254

.010 +.010

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

TRIBOW, REDUCING,

3/8" TO 1/4"

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278640

REV

SCALE: 4/1 SHEET: 2 OF 2

COPLANAR TO A

WITHIN .102 [.004]

SECTION A-A

SECTION B-B

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REVISION

DESCRIPTION ZONEREV

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE: CREO 3.0

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

.01

.XXX

.001

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

ELBOW, 1/4",

LONG LEG, REM

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278643

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278643 ELBOW, 1/4" LONG LEG, REM TI 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED".

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIMUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

L D

L I N E

F O L D

L I N E

REV 08/2016

16,669 0,254 .656 .010[ ]

29,369 0,254

1.156 .010[ ]

7,938 0,254 .313 .010[ ]

6,35 +0,102

.250 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

7,95 0,254 .313 .010[ ]

SR 2,464 0,051

.097 .002[ ]

2X 0,71 0,102 .028 .004[ ]

2X R0,254 +0,254

.010 +.010

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

ELBOW, 1/4",

LONG LEG, REM

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278643

REV

SCALE: 4/1 SHEET: 2 OF 2

SECTION A-A

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REVISION

DESCRIPTION ZONEREV

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE: CREO 3.0

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

.01

.XXX

.001

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

FITTING, ELBOW,

1/4", LOW PRESSURE

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278627

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278627 FITTING, ELBOW, 1/4" LP TITANIUM, 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED.

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

L D

L I N E

F O L D

L I N E

REV 08/2016

16,669 0,254 .656 .010[ ]

7,938 0,254 .313 .010[ ]

6,35 +0,102

.250 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

7,95 0,254 .313 .010[ ]

SR 2,464 0,051

.097 .002[ ]

2X 0,71 0,102 .028 .004[ ]

2X R0,254 +0,254

.010 +.010

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

FITTING, ELBOW,

1/4", LOW PRESSURE

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278627

REV

SCALE: 4/1 SHEET: 2 OF 2

SECTION A-A

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REVISION

DESCRIPTION ZONEREV

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE: CREO 3.0

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

.01

.XXX

.001

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

ELBOW, REDUCING,

3/8" TO 1/4"

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278638

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278638 ELBOW, REDUCING, 3/8" TO 1/4" TI 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED".

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIMUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

L D

L I N E

F O L D

L I N E

REV 08/2016

18,263 0,254 .719 .010[ ]

11,125 0,254 .438 .010[ ]

9,525 +0,102

.375 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

11,125 0,254 .438 .010[ ]

SR 4,051 0,051

.160 .002[ ]

0,71 0,102 .028 .004[ ]

2X R0,254 +0,254

.010 +.010

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

ELBOW, REDUCING,

3/8" TO 1/4"

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278638

REV

SCALE: 4/1 SHEET: 2 OF 2

SECTION A-A

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

Violations of these regulations are punishable by fine, imprisonment, or both.

L D

L I N E

F O L D

L I N E

REVISION

DESCRIPTION ZONEREV

METRIC/INCH

HARDWARE CLASSIFICATION

A METRIC

SOFTWARE:

PROGRAM:

LAST MODIFIED:03-Jun-19 04:11:08 PM

RELEASED STATE: Released

INCH BLOCK TOLERANCE: IN

.XX

.02

.XXX

.005

X/X 1/16

REMOVE ALL BURRS

AND SHARP EDGES

METRIC BLOCK TOLERANCE: MM

> 0 100 500 1000

< 100 500 1000 >1000

0.3 0.4 0.5 1.5

REMOVE ALL BURRS

AND SHARP EDGES

- EUROPA

NEXT ASSY USED ON

NATIONAL AERONAUTICS AND

SPACE ADMINISTRATION Goddard Space Flight Center GREENBELT, MD

WALLOPS ISLAND, VA

ELECTRONIC SIGNATURES ARE

AVAILABLE ONLINE AT:

https://gddms.gsfc.nasa.gov/Windchill

DRAWING INTERPRETED PER 500-PG-8700.2.5

TITLE

TRIBOW, 1/4",

FUEL/OXIDIZER

EUROPA PROPULSION SYSTEM

DESIGNER

K. WOLKO

CHECKER

D. FOOTE

ENGINEER-MECH

D. BENSON

ENGINEER-STRESS

S. CHAYKOVSKY

ENGINEER-QA

M. FOX

SIZE

CAGE CODE:

36FC1

DWG NO.

2278641

REV

APDL

C. BACHA SCALE: 4/1 SHEET: 1 OF 2

ITEM

NO. LIST OF MATERIAL

REQD REQD PART NO. DESCRIPTION MATERIAL / MATERIAL SPEC CAGE CODE

- X 2278641 TRIBOW, 1/4" TI 6AL-4V 36FC1

NOTES: UNLESS OTHERWISE SPECIFIED

1. DIMENSIONS ARE IN MM [INCHES]. ENGLISH DIMENSIONS

ARE FOR REFERENCE ONLY.

2. MATERIAL SHALL BE TITANIUM 6AL-4V BAR, ANNEALED

CONDITION, IN ACCORDANCE WITH SAE-AMS-4928 "TITANIUM ALLOY

BARS, FORGINGS, RINGS, AND DRAWN SHAPES, 6AL-4V, ANNEALED".

3. MATERIAL THICKNESS CROSS SECTION DIMENSIONS ARE NOT TO EXCEED

63.5mm [2.5 INCHES].

4. DISCARD ONE THICKNESS OF BAR EDGE MATERIAL (PARALLEL TO THE ROLLING

DIRECTION) TO PREVENT INCORPORATION OF EDGE DEFECTS.

5. THE VENDOR SHALL SUPPLY STOCK COUPONS TO GSFC: 25.4 MM [1.00 IN] LENGTH

FROM EACH END OF BAR OR BAR.

6. THE VENDOR SHALL PROVIDE MATERIAL CERTIFICATE OF CONFORMANCE.

7. THE VENDOR SHALL PROVIDE A DIMENSIONAL INSPECTION CERTIFICATION.

8. FINISH OF THE INSIDE PASSAGES AND OUTSIDE OF THE TUBE STUBS SHALL

BE 32 RA OR BETTER. FINISH OF THE OUTSIDE OF THE CUBE SHALL BE 63

RA OR BETTER.

9. CUTTING TOOLS SHALL NOT BE SiO2 OR SiO2 COATED.

10. NO BURRS, GOUGES, OR SCRATCHES ON ANY SURFACE, EXCEPT FOR PART

IDENTIFICATION.

LEAVE AS SHARP EDGE, HOWEVER, DEBURR AS NEEDED WITH R.051[.002 IN] MAX.

MARK EACH PART USING ELECTROCHEMICAL ETCHING IN ACCORDANCE WITH

MIL-STD-792 TYPE II ON THE CUBE BODY. INCLUDE THE DRAWING NUMBER

AND DASH NUMBER. MULTIPLE CUBE FACES MAY BE USED IF REQUIRED. THE

MAXIMUM DEPTH OF THE MARKING MAY NOT EXCEED .051[0.002 IN]. LASER

ENGRAVING (TYPE VIII) MAY BE USED WITH THE PERMISSION OF GSFC BUT MAY NOT

EXCEED THE MAXIMUM DEPTH OF .051[0.002 IN].

13. THE VENDOR SHALL DELIVER THE PARTS VISUALLY CLEAN AND INDIVIDUALLY

BAGGED IN RESEALABLE PACKAGES. PRECISION CLEANING, CLEANLINESS

VERIFICATION, AND BAGGING WILL BE ACCOMPLISHED BY GSFC.

14. EACH INDIVIDUAL PART WILL BE VISUALLY INSPECTED BY GSFC PRIOR TO

PRECISION CLEANING. INSPECT WITH A STEREO MICROSCOPE AT 20X

MAGNIFICATION OR BETTER. ALL EXTERIOR SURFACES WILL BE INSPECTED.

INTERIOR SURFACES WILL BE INSPECTED WITHIN THE LIMITS OF THE

EQUIPMENT (ONE ID MINIMUM DESIRED). ALL VOIDS, CRACKS, AND

LAMINATIONS WILL BE REPORTED.

15. PRECISION CLEANING, CLEANLINESS VERIFICATION, AND BAGGING WILL BE

ACCOMPLISHED BY GSFC IN ACCORDANCE WITH 597-WI-8700.2.1, "CLEANING

& ETCHING OF TITANIUM PROPULSION SYSTEM FLIGHT TUBING".

Released

MASTER DRAWING

GSFC FILE COPY

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

L D

L I N E

F O L D

L I N E

REV 08/2016

16,662 0,254 .656 .010[ ]

16,663 0,254 .656 .010[ ]

7,925 0,254 .312 .010[ ]

6,35 +0,102

.250 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

6,35 +0,102

.250 +.004 -.000[ ]

7,925 0,254 .312 .010[ ]

SR 2,464 0,051

.097 .002[ ]

3X 0,71 0,102 .028 .004[ ]

3X R0,254 +0,254

.010 +.010

REVISION

DESCRIPTION ZONEREV

INC EO 1 -A

TITLE

TRIBOW, 1/4",

FUEL/OXIDIZER

EUROPA PROPULSION SYSTEM

SIZE

CAGE CODE:

36FC1

DWG NO.

2278641

REV

SCALE: 4/1 SHEET: 2 OF 2

COPLANAR TO A

WITHIN .102 [.004]

SECTION A-A

SECTION B-B

EAR ECCN 9E515

- Export Administration Regulations (EAR) Notice -

2 V2.0 9-22

SECTION 2

INSTRUCTION TO OFFERORS

☒52.212-1 Instructions to Offerors – Commercial Items (Oct. 2018) Addendum to 52.212-1

Quotes for the item(s) described in the RFQ are due by 6/27/2019 by 2:00 p.m. CT to Dalonna Penton at Dalonna.d.penton@nasa.gov in order to be considered for award. If it is in the best interest of the Government, quotes submitted after the due date may be accepted. Quotes shall remain valid for 30 days unless otherwise expressly stated on the quote. Submitted Quotes shall list two points of contacts including name, phone number, and email address.

All contractual and technical questions must be in writing (e-mail) to Dalonna Penton at Dalonna.d.penton@nasa.gov no later than 6/26/2019 by 12:00 p.m. CT. Telephone questions shall not be accepted.

The NAICS Code for this procurement is 334511.

This procurement is set aside for small business.

Offeror’s shall be registered at www.sam.gov in order to be considered for award.

Delivery is FOB Destination.

SECTION 3

SOLICITATION PROVISION/REPRESENTATIONS AND CERTIFICATIONS

☒52.252-1 SOLICITATION PROVISIONS INCORPORATED BY REFERENCE (FEB 1998)

This solicitation incorporates one or more solicitation provisions by reference, with the same force and effect as if they were given in full text. Upon request, the Contracting Officer will make their full text available. The offeror is cautioned that the listed provisions may include blocks that must be completed by the offeror and submitted with its quotation or offer. In lieu of submitting the full text of those provisions, the offeror may identify the provision by paragraph identifier and provide the appropriate information with its quotation or offer. Also, the full text of a solicitation provision may be accessed electronically at this/these address(es):

FAR http://farsite.hill.af.mil/vffara.htm NFS http://farsite.hill.af.mil/vfnasaa.HTM http://www.sam.gov/ http://farsite.hill.af.mil/vffara.htm http://farsite.hill.af.mil/vfnasaa.HTM

3 V2.0 9-22

FEDERAL ACQUISITIONI REGULATION (FAR) PROVISIONS INCORPORATED BY

REFERENCE:

☒52.204-07 System for Award Management (Oct 2018) ☒52.204-16 Commercial and Government Entity Code Reporting (Jul 2016) ☒52.204-17 Ownership or Control of Offeror (Jul 2016) ☒52.209-02 Prohibition on Contracting with Inverted Domestic Corporations – Representation (Nov

2015) ☒52.225-25 Prohibition on Contracting with Entities Engaging in Sanctioned Activities Or

Transactions Relating to Iran – Representation and Certifications (Aug 2018) ☐52.223-1 Biobased Product Certification (May 2012)

FAR PROVISISIONS IN FULL TEXT:

☒52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS—COMMERCIAL ITEMS

(OCT. 2018)

The offeror shall complete only paragraphs (b) of this provision if the Offeror has completed the annual representations and certification electronically via the System for Award Management (SAM) Web site located at http://www.sam.gov/portal. If the Offeror has not completed the annual representations and certifications electronically, the Offeror shall complete only paragraphs (c) through (u) of this provision.

(a) Definitions. As used in this provision--

“Economically disadvantaged women-owned small business (EDWOSB) concern” means a small business concern that is at least 51 percent directly and unconditionally owned by, and the management and daily business operations of which are controlled by, one or more women who are citizens of the United States and who are economically disadvantaged in accordance with 13 CFR part 127. It automatically qualifies as a women-owned small business eligible under the WOSB Program.

“Forced or indentured child labor” means all work or service—

(6) Exacted from any person under the age of 18 under the menace of any penalty for its nonperformance and for which the worker does not offer himself voluntarily; or

(7) Performed by any person under the age of 18 pursuant to a contract the enforcement of which can be accomplished by process or penalties.

“Highest-level owner” means the entity that owns or controls an immediate owner of the offeror, or that owns or controls one or more entities that control an immediate owner of the offeror. No entity owns or exercises control of the highest level owner.

“Immediate owner” means an entity, other than the offeror, that has direct control of the offeror. Indicators of control include, but are not limited to, one or more of the following: Ownership or interlocking management, http://www.sam.gov/portal

4 V2.0 9-22 identity of interests among family members, shared facilities and equipment, and the common use of employees.

“Inverted domestic corporation,” means a foreign incorporated entity that meets the definition of an inverted domestic corporation under 6 U.S.C. 395(b), applied in accordance with the rules and definitions of 6 U.S.C.

395(c).

“Manufactured end product” means any end product in product and service codes (PSCs) 1000-9999, except—

(1) PSC 5510, Lumber and Related Basic Wood Materials;

(2) Product or Service Group (PSG) 87, Agricultural Supplies;

(3) PSG 88, Live Animals;

(4) PSG 89, Subsistence;

(5) PSC 9410, Crude Grades of Plant Materials;

(6) PSC 9430, Miscellaneous Crude Animal Products, Inedible;

(7) PSC 9440, Miscellaneous Crude Agricultural and Forestry Products;

(8) PSC 9610, Ores;

(9) PSC 9620, Minerals, Natural and Synthetic; and

(10) PSC 9630, Additive Metal Materials.

“Place of manufacture” means the place where an end product is assembled out of components, or otherwise made or processed from raw materials into the finished product that is to be provided to the Government. If a product is disassembled and reassembled, the place of reassembly is not the place of manufacture.

“Predecessor” means an entity that is replaced by a successor and includes any predecessors of the predecessor.

“Restricted business operations” means business operations in Sudan that include power production activities, mineral extraction activities, oil-related activities, or the production of military equipment, as those terms are defined in the Sudan Accountability and Divestment Act of 2007 (Pub. L. 110-174). Restricted business operations do not include business operations that the person (as that term is defined in Section 2 of the Sudan Accountability and Divestment Act of 2007) conducting the business can demonstrate—

(1) Are conducted under contract directly and exclusively with the regional government of southern Sudan;

(2) Are conducted pursuant to specific authorization from the Office of Foreign Assets Control in the Department of the Treasury, or are expressly exempted under Federal law from the requirement to be conducted under such authorization;

(3) Consist of providing goods or services to marginalized populations of Sudan;

5 V2.0 9-22

(4) Consist of providing goods or services to an internationally recognized peacekeeping force or humanitarian organization;

(5) Consist of providing goods or services that are used only to promote health or education; or

(6) Have been voluntarily suspended.

Sensitive technology—

(1) Means hardware, software, telecommunications equipment, or any other technology that is to be used specifically—

(i) To restrict the free flow of unbiased information in Iran; or

(ii) To disrupt, monitor, or otherwise restrict speech of the people of Iran; and

(2) Does not include information or informational materials the export of which the President does not have the authority to regulate or prohibit pursuant to section 203(b)(3) of the International Emergency Economic Powers Act (50 U.S.C. 1702(b)(3)).

“Service-disabled veteran-owned small business concern”—

(1) Means a small business concern—

(i) Not less than 51 percent of which is owned by one or more service-disabled veterans or, in the case of any publicly owned business, not less than 51 percent of the stock of which is owned by one or more service-disabled veterans; and

(ii) The management and daily business operations of which are controlled by one or more service-disabled veterans or, in the case of a service-disabled veteran with permanent and severe disability, the spouse or permanent caregiver of such veteran.

(2) Service-disabled veteran means a veteran, as defined in 38 U.S.C. 101(2), with a disability that is service-connected, as defined in 38 U.S.C. 101(16).

“Small business concern” means a concern, including its affiliates, that is independently owned and operated, not dominant in the field of operation in which it is bidding on Government contracts, and qualified as a small business under the criteria in 13 CFR Part 121 and size standards in this solicitation.

“Small disadvantaged business concern, consistent with 13 CFR 124.1002,” means a small business concern under the size standard applicable to the acquisition, that--

(1) Is at least 51 percent unconditionally and directly owned (as defined at 13 CFR 124.105) by--

(i) One or more socially disadvantaged (as defined at 13 CFR 124.103) and economically disadvantaged (as defined at 13 CFR 124.104) individuals who are citizens of the United States;

and

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(ii) Each individual claiming economic disadvantage has a net worth not exceeding $750,000 after taking into account the applicable exclusions set forth at 13 CFR 124.104(c)(2); and

(2) The management and daily business operations of which are controlled (as defined at 13.CFR 124.106) by individuals, who meet the criteria in paragraphs (1)(i) and (ii) of this definition.

“Subsidiary” means an entity in which more than 50 percent of the entity is owned—

(1) Directly by a parent corporation; or

(2) Through another subsidiary of a parent corporation.

“Successor” means an entity that has replaced a predecessor by acquiring the assets and carrying out the affairs of the predecessor under a new name (often through acquisition or merger). The term “successor” does not include new offices/divisions of the same company or a company that only changes its name. The extent of the responsibility of the successor for the liabilities of the predecessor may vary, depending on State law and specific circumstances.

“Veteran-owned small business concern” means a small business concern—

(1) Not less than 51 percent of which is owned by one or more veterans(as defined at 38 U.S.C. 101(2)) or, in the case of any publicly owned business, not less than 51 percent of the stock of which is owned by one or more veterans; and

(2) The management and daily business operations of which are controlled by one or more veterans.

“Women-owned business concern” means a concern which is at least 51 percent owned by one or more women;

or in the case of any publicly owned business, at least 51 percent of the its stock is owned by one or more women; and whose management and daily business operations are controlled by one or more women.

“Women-owned small business concern” means a small business concern --

(1) That is at least 51 percent owned by one or more women or, in the case of any…

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