SATPC0008488_Tab_12_RFQ_Open_Market.pdf

National Aeronautics and Space Administration

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

2/1/2018

SUBJECT: Request for Quotation (RFQ) 80NSSC18Q0277, Electron Beam Welding

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

Mars Entry, Descent and Landing Instrumentation (MEDLI2)

Supersonic Sensor Electron Beam Welding Statement of Work, Deliverable Item List &

Schedule

MEDLI2-4047

Version 1

LANGLEY RESEARCH

CENTER

Hampton, Virginia

Table of Contents

1 General Information

1.1 Scope

1.2 Applicable Documents

2 Management, Reporting, Reviews, and documentation

2.1 Program management

2.2 Advanced Notifications

2.3 Reviews And Meetings

2.3.1 Weld Readiness Review

2.4 Documentation

2.4.1 General

2.4.2 Monthly Report

3 WeldING Qualification and flight

3.1 pathfinder SENSOR

3.1.1 Pathfinder Weld Schedule and Performance Qualification

3.1.2 Pathfinder Visual Inspection

3.1.3 Pathfinder Penetrant Testing

3.1.4 External Leakage

3.1.5 Pathfinder Metallographic Examination

3.2 Flight welding

3.2.1 Flight Units Class A Weld’s

3.2.2 Flight Units Class C Weld’s

3.2.3 Flight Units Visual A Class Weld’s

3.2.4 External Leakage

3.2.5 Flight Units Penetrant Testing

3.2.6 Cleanliness

3.3 government Test Area

3.4 Measurement and Test Equipment

3.4.1 Failure During Tests

3.4.2 Modification of Hardware

4 Quality Assurance

4.1 GENERAL REQUIREMENTS

4.1.1 Quality Assurance Plan/Manual

4.1.2 Surveillance of the Contractor

4.1.3 Anomaly Reporting

4.1.4 Configuration Management

4.2 STANDARDS AND PROCESSES

4.2.1 Standards Requirements

4.2.2 Electrostatic Discharge Control Requirements

4.2.3 Hardware Handling, Cleaning, and Packaging

4.2.4 Workmanship: Use of Alternate Workmanship Standards

4.3 Materials, Processes Requirements

4.3.1 Welding

4.3.2 Cleanliness

5 Handling, Storage, Packaging, Preservation, and Delivery 6 Appendix A. Abbreviations and Acronyms 7 Appendix B. MEDLI2 WELD Schedule 8 Appendix C. Deliverable Item List & Schedule (DILS)

8.1 Proprietary Data

8.2 DELIVERABLES

List of Tables

Table Page

Table 8-1 HARDWARE DELIVERY AND SCHEDULE Table 8-2 DATA DELIVERY DOCUMENTATION AND SCHEDULE

1 General Information

NASA intends on collecting low pressure data on a future Mars entry mission. These pressure measurements will be collected using a custom pressure transducer which is capable of surviving the extreme space environments.

1.1 Scope

This document defines the work to be performed by the contracted welder for the welding and weld qualification of the Mars Entry, Descent, and Landing Instrumentation 2 (MEDLI2) supersonic pressure transducers. The contractor shall provide the facilities, personnel, services, tools, equipment, and materials necessary to test, and deliver the services and data in accordance with the requirements of this Statement of Work (SOW) and the appendices.

1.2 Applicable Documents

All applicable and reference documentation identified in this document shall apply in the situations where they are specifically referenced. In the event of a conflict between the SOW and the standards, the SOW shall take precedence.

2 Management, Reporting, Reviews, and documentation

2.1 Program management

The contractor shall designate an individual(s) who will be given full responsibility and authority to manage and administer all phases of the work specified by the contract and ensure that all objectives are accomplished within schedule constraints.

2.2 Advanced Notifications

The contractor shall notify the NASA/LaRC TECHNICAL END USER at least seven (7) calendar days in advance of all mandatory hardware inspections, test activities, Technical Interchange Meetings, and deliveries at either the contractor’s or a sub-contractor’s facility to allow timely participation by the NASA/LARC Quality Assurance representative. Event specific notification requirements (such as failures, anomalies, etc.) are included in the appropriate sections.

2.3 Reviews And Meetings

2.3.1 Weld Readiness Review

The Contractor shall organize and conduct a Weld Readiness Review at the Contractor’s facility prior to conducting any weld or NDE any activities identified in this SOW within thirty (30) calendar days after award of the contract.

The Contractor shall provide the review content at least five (5) calendar days prior to the review.

The Weld Readiness Review shall address program management, heritage of the processes to be used, and quality assurance activities outlined in this SOW. At a minimum, the Weld Readiness Review presentation content shall address the following areas:

• Program Management

• Quality Assurance

• Initial Program Schedule Release

• Manufacturing flow with government mandatory inspection points (section 4.1.2.3)

• Facilities

• Status of certifications

• Review of outside services planned and Status of certifications

• Review of approach for internal tests (leak testing)

• Review of metallographic inspection procedure

• Cleanliness Procedures

• ESD Procedures

2.4 Documentation

2.4.1 General

The contractor shall ensure the generation and delivery of all documentation as specified in this SOW and Appendix D.

In addition to that documentation specifically called for in the contract, upon request by the NASA/LaRC TECHNICAL END USER, the contractor shall make available a copy of any document or data generated during this contract performance for review by LaRC at either the contractor's facility or via the internet. This includes, but is not limited to, technical reports and memorandums, drawings, parts and materials data, test data, etc.

2.4.2 Monthly Report

The contractor shall provide a report on the overall status of the tasks and activities to the Government on a monthly basis. The report shall be provided electronically. The format of the monthly report is at the discretion of the contractor (can be an email with the content included or an attached document). The report shall emphasize the technical status and progress including anomaly resolution, significant completions, and schedule status.

3 WeldING Qualification and flight

3.1 pathfinder SENSOR

NASA LaRC will designate one sensor to be a weld qualification sensor (Pathfinder Sensor). This sensor will have an identical envelope and weld design as the flight sensors. This sensor will precede the flight units and provide confirmation that weld schedule meets the requirements of the MEADS Weld detail drawings (Drawing numbers: 1300378, 1300379, and 1300380), AWS D17.1, and this statement of work MEDLI2-4047. The pathfinder shall also be used for procedure verification and qualification for visual inspection, penetrant inspection, leak testing, and metallographic examination.

3.1.1 Pathfinder Weld Schedule and Performance Qualification

The pathfinder sensor will establish the requirements for weld schedule development, welding procedure qualification, and welder/welding operator/tack welder performance qualification. The weld schedule developed and verified through the pathfinder approach shall become the baseline approach for the flight sensors. The weld schedule shall be compliant with AWS D17.1 for the development of weld procedure specifications (Note appendix B is provided as an example of a weld schedule).

3.1.2 Pathfinder Visual Inspection

The pathfinder shall be used for verification of the visual inspection requirements and inspection procedure for each weld. Visual inspection requirements for each weld shall meet the requirements of AWS D17.1 for Class A welds (with the exception of drawing 1300379 Note 7 and Note 9, the Tack weld shall meet the Class C requirements). The visual inspection procedure shall be submitted to the government and approved by the government prior to the execution of flight welding.

Prior to performing the final body weld, the contractor shall provide images of each weld completed (per drawings 1300379 and 1300380). The weld images shall be the full circumference of each weld (multiple images are acceptable to provide full coverage of the weld). The images shall be provided to the Government Technical User either via e-mail or posting on a server available to both the Contractor and the Government.

Upon completion of the final body weld (drawing 1300378), the contractor shall provide images of the final weld. The weld images shall be the full circumference of the weld (multiple images are acceptable to provide full coverage of the weld). The images shall be provided to the Government Technical User either via e-mail or posting on a server available to both the Contractor and the Government.

3.1.3 Pathfinder Penetrant Testing

The pathfinder shall be used for verification of the penetrant test requirements and test procedure for each weld. Penetrant test requirements for each welded sub-assembly shall meet ASTM E1417. The penetrant test procedure shall be submitted to the government and approved by the government prior to the performance of penetrant testing of the welds.

3.1.4 External Leakage

With the sensors pressure port capped off (sealed) the sensor will be exposed to 15 PSIG of gaseous helium while sealed in a hermetic chamber for a minimum of 60 minutes. Then the sensor will be removed from the chamber and using a helium leak detector sniffed for trace helium around the welds. After welding the external leakage shall not exceed 1*10-6 cc/s.

The pathfinder sensor shall be used for development of the External Leakage test requirements and test procedure for the sensor sub-assembly and final sensor assembly. The leak test procedure shall be performed in accordance with MIL-STD-883 (latest revision) and require the TECHNICAL END USER approval.

3.1.5 Pathfinder Metallographic Examination

After the pathfinder sensor has been fully welded, visual and penetrant testing completed, and external leakage testing completed, then a metallographic examination of the welds shall be performed. The sensor shall be cut into four sections to evaluated (8 surfaces). The welds to be evaluated shall be 1300379 Note 5, 1300378 Note 4, 1300279 Note 7, and 1300380 Note 4. After the sensor is cut, then the metallographic examination of the exposed weld cross-sections shall be performed using magnification of 5X–100X (drawing number 1300378 “SUPERSONIC

PRESSURE TRANSDUCER

WELDING DETAILS”).

3.2 Flight welding

Forty four (44) flight sensors will trail the pathfinder qualification unit. The flight units will utilize the weld schedules baselined during the pathfinder qualification.

3.2.1 Flight Units Class A Weld’s

The following welds are to be performed on 44 MEDLI2 supersonic pressure sensors to the Class A Requirements of AWS D17.1 using an Electron Beam Welder:

• Drawing 1300379 Note 6

• Drawing 1300379 Note 8

• Drawing 1300380 Note 5

• Drawing 1300378 Note 5

3.2.2 Flight Units Class C Weld’s

The following welds are to be performed on 44 MEDLI2 supersonic pressure sensors to the Class C Requirements of AWS D17.1:

• Drawing 1300379 Note 7

• Drawing 1300379 Note 9

3.2.3 Flight Units Visual A Class Weld’s

Visual inspection shall be in accordance with AWS D17.1 for each weld. The approved pathfinder procedure shall be use along with NASA drawing number 1300378, 1300379, and 1300380 for inspection.

3.2.4 External Leakage

The external leakage test developed from 3.1.4 shall be performed on each sensor. External leakage shall not exceed 1*10-6 cc/s.

3.2.5 Flight Units Penetrant Testing

Penetrant Testing shall be performed on each sub-assembly per ASTM E1417 for class A welds.

The approved pathfinder procedure shall be use along with NASA drawing number 1300378, 1300379, and 1300380 for inspection.

3.2.6 Cleanliness

Welds identified as requiring contamination controls shall be handled as follows:

LaRC provided attire must be worn at all times while working with these sensors. Which includes but is not limited to the following:

• Cleanroom Smock

• Gloves

• Hairnets

• Beard Covers

The sensors shall remain sealed until welding is to occur to minimize exposure time in a non-cleanroom environment. The sensors shall not be removed from their sealed packaging without LaRC personnel present. LaRC provided contamination witness plates will accompany the transducers in the pre-area and inside the welding chamber.

Plates may be changed out, covered and uncovered at the direction of LaRC personnel.

At the start of each welding shift, the EB chamber shall be cleaned using in 99.9% HPLC spectrographic grade IPA. A contamination witness sample will be placed in the EB chamber after cleaning and pumped down to minimum of 1*10-3 torr and held for five minutes. The contamination witness sample will then be removed and analyzed by LaRC personnel.

Welds requiring contamination witness samples are as follows:

• Drawing 1300379 Note 6

• Drawing 1300379 Note 8

• Drawing 1300378 Note 5

• Drawing 1300379 Note 7

• Drawing 1300379 Note 9

3.3 government Test Area

The government will conduct measurements at the contractor’s facility prior to performing the welding shown on drawing 1300379 note 7 as well as repeating the same measurements at the conclusion of the welding shown on drawing 1300379 note 9. The contractor shall make available to the government an ESD secure area during the execution of the welding per 1300379 to perform the measurements of the internal components. The ESD secured area shall have at a minimum 2 electrical outputs and one ESD Safe bench. The government will provide all other test equipment needed to perform these measurements. It is anticipated that the ESD secure area will be needed for up to 3 working days.

3.4 Measurement and Test Equipment

All measurement and test equipment used for calibration and/or verification of a requirement shall comply with the American National Standard for Calibration of Measurement and Test Equipment ANSI/NCSL Z540.3-2006 or equivalent.

3.4.1 Failure During Tests

When a failure (non-conformance or trend indicating that an out-of-spec condition will result) occurs, determination will be made as to the feasibility and value of continuing the test to its specified conclusion. The test shall be stopped if equipment fails during testing in cases where this failure will result in damage to the pressure sensors. Otherwise, the test shall be completed to obtain as much information as possible. If corrective action is taken, the test will be repeated to the extent necessary to demonstrate that the test item’s performance is satisfactory. If corrective action taken as a result of failure affects the validity of previously completed tests (e.g., redesign of a component), prior tests will be repeated.

No replacement, adjustment, maintenance, or repairs are authorized during testing except external cleaning is allowed before cleanliness verification. This requirement does not prevent the replacement or adjustment of equipment that has exceeded its design operating life during tests, provided that after such replacement, the equipment is tested as necessary to assure its proper operation. A complete record of any exceptions taken to this requirement shall be included in the test report.

3.4.2 Modification of Hardware

Once external leakage test has started, no alteration to the test configuration is to be permitted that might alter the test data results from the flight units under test. This includes cleaning, adjustment or re-calibration for all the test equipment involved with the external leakage test configuration setup.

4 Quality Assurance

4.1 GENERAL REQUIREMENTS

4.1.1 Quality Assurance Plan/Manual

The contractor shall have a Quality Management System that is compliant with the requirements of SAE AS9100 Quality Systems – Aerospace – Model for Quality Assurance in Design, Development, Production, Installation and Servicing.

4.1.2 Surveillance of the Contractor

The work activities and operations of the contractor, subcontractors, and suppliers are subject to evaluation, review, survey, and inspection by a LaRC representative.

The contractor shall provide the LaRC representative with documents, records, equipment, and workings areas within their facilities that are required by the representative to perform their overview activities.

4.1.2.1 Government Source Inspection

The Government may elect to perform inspections at a supplier's facilities. The following statement shall be included on all procurement documents: “All work on this order is subject to inspection and test by the Government at any time and place.”

The Government quality representative who has been delegated NASA quality assurance functions on this procurement shall be notified within 2 business days upon contractor receipt of any supplier/subcontractor orders. The Government representative shall also be notified 48 hours in advance of the time that articles or materials are ready for inspection or test.

4.1.2.2 Contractor Source Inspection

The contractor shall ensure that its procurement documents impose the applicable requirements on subcontractors and other suppliers. The subcontractor and other suppliers shall in turn impose the requirements on their procurement sources.

The contractor shall perform source inspection at the subcontractor's or supplier's facilities in accordance with the procurement documentation or when one or more of the following conditions exist:

• In process, end item controls, or tests that are destructive in nature prevent the contractor from verifying quality after delivery to the contractor's facility.

• It is not feasible or economical for the contractor to determine the quality of procured articles solely by inspections or tests performed at the contractor’s facility.

4.1.2.3 Government Mandatory Inspection Points (MIPs)

The government intends on conducting [three (3)] Mandatory Inspection Points (MIPs) in addition to the reviews noted elsewhere for this procurement.

MIP-1: The first MIP planned by the Government is during the welding performed for drawing 1300379. The Government will be at the contractor’s facility during the period that the welding is performed for drawing 1300379 to conduct the measurements of the internal components (see paragraph 3.3).

MIP-2: The second MIP planned by the Government is at the completion of the External Leakage test (see paragraph 3.2.3) of the flight units. The government will review the results of the External Leakage test prior to acceptance of these units and before any weld repairs are conducted.

MIP-3: The timing and description of this MIP is TBD and will be determined during the Welding Readiness Review.

After contract award, the Government may change these MIPs based on discussions with the contractor. The MIPs will be baselined at the Welding Readiness Review.

In the event that proper notification has been made and 48 hours have elapsed without the MIP being accomplished, the contractor can waive the MIP after receiving NASA/LaRC TECHNICAL END USER approval.

4.1.3 Anomaly Reporting

The NASA LaRC TECHNICAL END USER shall be notified within 24 hours of each anomaly observed.

The contractor’s processes for review, disposition and approval of anomaly reports shall be described in their quality plan/manual or provided as a supplemental document. In addition, the contractor’s anomaly reporting document shall describe the members of the Material Review Board (MRB) and Failure Review Board (FRB). The MRB and FRB for any MEDLI2 pressure transducer anomalies shall include MEDLI2 LaRC participation.

The contractor shall provide the NASA LaRC Technical End User notice of MRB or FRB meetings related to MEDLI2 pressure transducer anomalies with at least 24 hours’ notice of the meeting.

The NASA LaRC Technical End User may participate in the MRB or FRB meetings either remotely or in person at the contractor’s facility depending on the nature of the anomaly and the amount of notice available.

The contractor shall provide, as part of the monthly report, a list of all open anomaly reports and a separate list of the anomaly reports closed during the month. For each reported anomaly or nonconformance, there shall be a report that documents the investigation and engineering analysis needed to determine the cause and corrective actions to disposition the nonconformance, and identify any closed problem reports that do not have a definitive cause or corrective action. Reports shall be submitted to the NASA LaRC TECHNICAL END USER for review and approval of the disposition.

4.1.4 Configuration Management

The contractor shall have a Configuration Management (CM) system used to ensure the welding, inspection, and test approaches are defined and changes are controlled. The contractor’s CM system shall be available for review by the LaRC Technical End User, upon request.

All changes to the welding approach, inspection approach, or testing approach, shall be submitted to the NASA LaRC Technical End User for approval prior to implementation of the change. NASA LaRC Technical End User will provide a response within two (2) business days of receipt of the request for approval.

All other changes shall be controlled and dispositioned by the contractor. NASA LaRC Technical End User reserves the right to review all other changes to the MEDLI2 Pressure Transducer documents for technical content. Any flight item that is found to be non-compliant with the quality, workmanship, inspection, and/or test requirements of the contract shall be dispositioned via a waiver or MRB, unless the affected item is reworked to restore compliance. The contractor shall submit waivers to the NASA LaRC TECHNICAL END USER for final approval.

4.2 STANDARDS AND PROCESSES

The contractor’s efforts shall fully encompass the specific requirements of this chapter during execution of this SOW. It is the contractor’s responsibility to list all deviations from the baseline workmanship standards and to provide data supporting their position/rationale.

4.2.1 Standards Requirements

The following standards shall apply.

• Metallographic Inspection, Electron Beam Welding & Tack Welding: AWS D17.1, Specification for Fusion Welding for Aerospace Applications

• Penetrant Testing: ASTM E1417M, Standard Practice for Liquid Penetrant Testing;

• AWS A2.4, Standard Symbols for Welding, Brazing, and Nondestructive Examination;

• AWS A3.0M/A3.0, Standard Welding Terms and Definitions Including Terms for

Adhesive Bonding, Brazing, Soldering, Thermal Cutting, and Thermal Spraying;

• AWS B2.1/B2.1M, Specification for Welding Procedure and Performance Qualification;

• AWS B4.0, Standard Methods for Mechanical Testing of Welds;

• AWS B5.2, Specification for the Qualification of Welding Inspectors Specialists and

Welding Inspector Assistants;

• AWS QC1, Standard for AWS Certification of Welding Inspectors

4.2.2 Electrostatic Discharge Control Requirements

The contractor shall document and implement an Electrostatic Discharge (ESD) Control Program suitable to protect ESD-sensitive components at all levels of assembly and integration. This procedure shall be made available to the NASA LaRC Technical End User for review.

4.2.3 Hardware Handling, Cleaning, and Packaging

The handling of flight hardware shall be performed by qualified personnel in accordance with approved procedures that address cleaning, handling, packaging, tent enclosures, shipping containers, bagging, and purging. Compatible packaging shall be selected so that hardware is not contaminated or otherwise degraded during shipping or storage. All personnel working on flight hardware shall be certified as having completed the required training and competency certifications prior to handling any flight hardware. This includes, but is not limited to, workmanship, clean room and ESD awareness courses.

4.2.4 Workmanship: Use of Alternate Workmanship Standards

LARC recognizes that the contractor may have an established workmanship program equivalent to the specific standards cited herein. In these instances, the contractor may use existing standards upon review and approval by the MEDLI2 Project TECHNICAL END USER. It must be established that the contractor’s workmanship program fully encompasses the specific requirements of this chapter. It is the contractor’s responsibility to list all deviations from the baseline workmanship standards and to provide data supporting their position/rationale.

4.3 Materials, Processes Requirements

4.3.1 Welding

Welding shall be performed and inspected per contractor and NASA approved procedure according to AWS D17.1. Control of weld filler material shall also be per contractor and NASA approval. Test records for the visual inspections, liquid penetrant testing, and the external leakage testing shall all be retained. At a minimum, the Contractor shall maintain a heritage internal process that contains a weld schedule including settings and configuration demonstrating a repeatable performance.

4.3.2 Cleanliness

All hardware cleanliness shall be in accordance paragraph 3.2.6.

5 Handling, Storage, Packaging, Preservation, and Delivery

Products shall be stored, preserved, marked, labeled, and packaged to prevent loss of marking, deterioration, contamination, excessive condensation and moisture, or damage during all phases of the program.

The contractor shall reuse the shipping container used to ship the LaRC components to the contractor for shipping the completed sub-assemblies back to LaRC.

6 Appendix A. Abbreviations and Acronyms

Abbreviation/ Acronym Definition

A Approve ANSI American National Standards Institute CM Configuration Management CO Contracting Officer DILS Deliverable Item List & Schedule EDL Entry, Descent, and Landing EEE Electrical, Electronic, and Electromechanical ESD Electrostatic-Discharge I Information LaRC Langley Research Center MEADS Mars Entry Atmospheric Data System MEDLI2 Mars Entry, Descent, and Landing Instrumentation 2 MIP Mandatory Inspection Point MRB Material Review Board NASA National Aeronautics and Space Administration Pa Pascal PSIA Pounds per Square Inch (Absolute) QA Quality Assurance R Review SOW Statement of Work

14 V2.0 9-22

7 Appendix B. MEDLI2 WELD Schedule

MEDLI2: Supersonic Pressure Sensor WELD SCHEDULE DWG: 1300380 Note 4

SUPERSONIC SENSOR CONNECTOR, MEASDS: WELD DETAIL CONNECTOR Body to

CONNECTOR

COMPANY NAME BY

SUPPORTING PQR Nos.

WELDING PROCESS: Electron Beam Welding TYPE Manual, Semi-Automatic, Automatic, Robotic

JOINTS

JOINT TYPE Fillet Weld in Tube/ Butt Weld

BACKING NONE

BACKING MATERIAL (TYPE) NONE

Notes: PER NASA DRAWG: 1300380 NOTE 4

Sketches, production drawings, welding symbols, or written description should show the general arrangement of the parts to be welded. Where applicable, the root spacing details of the weld groove may be specified.

BASE METAL(S)

M-No. 8 GROUP No. 1 TO M-No. 8 GROUP No. 1

SPECIFICATION TYPE AND GRADE S304L

A240

TO SPECIFICATION TYPE AND GRADE S304L A240

THICKNESS RANGE

OF BASE METAL GROOVE FILLET 0.035” FLANGE

PIPE DIA. RANGE GROOVE FILLET 0.0785”

OTHER

FILLER METALS

FILLER METAL F-No. OTHER

AWS CLASSIFICATION

AWS SPECIFICATION

FILLER METAL SIZE

OTHER

Joint Details

15 V2.0 9-22

Weld Schedule (MEDLI2 MEADS) WS NUMBER (PAGE 2) 1300380 NOTE 4

POSITIONS

POSITION(S) OF GROOVE WELD PROGRESSION

POSITION(S) OF FILLET

PREHEAT

PREHEAT TEMP. (MINIMUM) INTERPASS TEMP. (MAXIMUM)

PREHEAT MAINTENANCE

CONTINUOUS OR SPECIAL HEATING OR MAINTENANCE

ELECTRICAL CHARACTERISTICS

CURRENT TYPE AND POLARITY PULSING (YES OR NO)

CURRENT (RANGE) VOLTAGE (RANGE)

WIRE FEED SPEED (RANGE)

PULSING PARAMETERS

OTHER

OTHER VARIABLES

CUP OR NOZZLE SIZE COLLET BODY OR GAS LENS

CLEANING METHOD

NUMBER OF ELECTRODES

OTHER

WELDING PARAMETERS

LAYERS PROCESS

VACUUM FILLER METAL ELECTRICAL TRAVEL

SPEED

RANGE

Pressure (torr) Class Diameter Type &

Polarity Current Range

Voltage Range

16 V2.0 9-22

8 Appendix C. Deliverable Item List & Schedule (DILS)

8.1 Proprietary Data

In the event data is deemed to be proprietary, and for which protection is to be maintained, the sending Party shall mark the document with a notice to indicate that the data therein is proprietary and shall be used and disclosed by the receiving Party and its related entities (e.g., contractors and subcontractors) only for the purposes of fulfilling the receiving Party’s responsibilities under the Mars Entry, Descent and Landing Instrumentation (MEDLI2) Project. The identified and marked technical data shall not be disclosed or retransferred to any other entity without prior written permission of the document preparer.

8.2 DELIVERABLES

Description: This provides the “Title” of the deliverable item.

Reference: This provides the reference back to the pertinent document calling out the deliverable.

Category:

A = Approval – Items in this category requires approval from the National Aeronautics and Space Administration (NASA)/Langley Research Center (LaRC) Technical End User.

Documents shall be provided in contractor format as long as required content, as specified in the Mars Entry, Descent, and Landing Instrumentation (MEDLI2) Project Pressure Transducer Statement of Work (MEDLI2-6006), is addressed. The NASA LaRC Technical End User reserves the time-limited right of disapproval for each submission. The time-limited period is five business days from receipt of documents.

R= Review – Items in this category do not require formal NASA LaRC Technical End User approval, but will be reviewed by LaRC or its designated representatives in order to determine contractor effectiveness in meeting contract objectives. When Government review reveals inadequacies, the contractor may be requested to correct the inadequacies. LaRC shall review and comment within five business days of receipt.

I = Information – Items in this category are informal and are for information only.

S = Service – Items in this category are services performed complete skilled processes for the government.

Quantity: This provides the required number of copies for the deliverable. For documents, the following formats apply:

H = Hardcopy – Provide a reproducible hardcopy of submittal to NASA/LaRC.

E = Electronic – Provide submittal in electronic format to the Mars Entry, Descent, and Landing Instrumentation (MEDLI2) Project Library, TECHNICAL END USER, and Contracting Officer

17 V2.0 9-22

Table 8-1 HARDWARE DELIVERY AND SCHEDULE

Item

Description Ref. Category Quantity Delivery Date

1 Electron Beam (EB) Welding of flight sensors per 1300380 SUPERSONIC

SENSOR CONECTOR

MEADS: WELD DETAIL

SOW

3.2.1

S 44 03/05/18

2 Penetrant Testing per 1300380

SUPERSONIC SENSOR CONECTOR

MEADS: WELD DETAIL

SOW

3.2.5

S 44 03/05/18

3 Electron Beam (EB) Welding of flight sensors per 1300379 SUPER SONIC

SENSOR ASSEMBLY MEASDS:

WELD DETAIL

SOW

S 44 03/29/18

4 Gaseous Helium Leak Test per 1300379

SUPER SONIC SENSOR ASSEMBLY

MEASDS: WELD DETAIL

SOW

3.2.4

5 Penetrant Testing per 1300379 SUPER

SONIC SENSOR ASSEMBLY

MEASDS: WELD DETAIL

SOW

3.2.5

S 44 03/29/18

6 Electron Beam (EB) Welding of flight sensors per 1300378 SUPERSONIC

PRESSURE TRANSDUCER

MEADS: WELDING DETAILS

SOW

7 Penetrant Testing per 1300378

SUPERSONIC PRESSURE

TRANSDUCER

MEADS: WELDING DETAILS

SOW

3.2.5

8 Gaseous Helium Leak Test per 1300378

TRANSDUCER

MEADS: WELDING DETAILS

SOW

3.2.4

9 Electron Beam (EB) Welding of non-flight pathfinder sensor per 1300380

SUPERSONIC SENSOR CONECTOR

MEADS: WELD DETAIL

SOW

3.1.1

S 1 03/05/18

10 Penetrant Testing per 1300380

SUPERSONIC SENSOR CONECTOR

for non-flight pathfinder sensor

MEADS: WELD DETAIL

SOW

3.1.3

S 1 03/05/18

11 Electron Beam (EB) Welding of non-flight pathfinder sensors per 1300379

SUPER SONIC SENSOR ASSEMBLY

MEADS: WELD DETAIL

SOW

S 1 03/29/18

12 Gaseous Helium Leak Test per 1300379

SUPER SONIC SENSOR ASSEMBLY

for non-flight pathfinder sensor

MEADS: WELD DETAIL

SOW

3.1.4

18 V2.0 9-22

Description Ref. Category Quantity Delivery Date

13 Penetrant Testing per 1300379 SUPER SONIC SENSOR ASSEMBLY for non-flight pathfinder sensor

MEADS: WELD DETAIL

SOW

14 Electron Beam (EB) Welding of non-flight pathfinder sensor per 1300378

SUPERSONIC PRESSURE

TRANSDUCER

MEADS: WELDING DETAILS

SOW

15 Gaseous Helium Leak Test per 1300378

TRANSDUCER non-flight pathfinder sensor

MEADS: WELDING DETAILS

SOW

3.1.4

16 Penetrant Testing per 1300378

TRANSDUCER non-flight pathfinder sensor

MEADS: WELDING DETAILS

SOW

17 Metallographic Examination of non-flight pathfinder sensor per 1300378

SUPERSONIC PRESSURE

TRANSDUCER

MEADS: WELDING DETAILS

SOW

3.1.5

18 Facilities for performing post weld check-out.

SOW

3.3

A 1 TBD

19 V2.0 9-22

Table 8-2 DATA DELIVERY DOCUMENTATION AND SCHEDULE

Description Reference Category Quantity Delivery Date

19 Weld Schedule SOW 3.1.5 R N/A 03/29/18

20 Certification Status SOW 2.3.1 R N/A 03/05/18

21 Penetrant Inspection Report SOW 3.2.5 A N/A 03/29/18

22 Metallographic Examination Report SOW 3.1.5 A N/A 03/29/18

23 Visual Examination Report SOW 3.2.3 A N/A 03/29/18

24 Monthly Report SOW 2.4.2 A N/A Monthly status report by email

8 7 6 5 4 3 1

12345678

A

B

C

DD

C

B

A

CAGE DWG. NO. SH REV.

NATIONAL AERONAUTICS & SPACE ADMINISTRATION

LANGLEY RESEARCH CENTER

HAMPTON, VA 23681-2199

TITLE

DWG.

NO.

CAGE CODESIZE REV.

SHEETSCALE

ACT. WT.CALC. WT.

DRAWN

CHECKED

DESIGNER

LEAD ENGR

BRANCH

SPECIAL MARKING SYMSIMILAR TO

FINISH

TREATMENT

DO NOT SCALE DRAWING

APPROVALS DATE

CONTRACT NO.UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES.

TOLERANCES

DECIMALS ANGULAR

.XX .03 .X .5

.XXX .010

1 OF 11/1

-130038025305D

MEADS SUPERSONINC TRANSDUCER

CONNECTOR WELDING DETAIL

25305CONNECTOR_BODY_WELD1 -

ALL SHEETS ARE REV LEVEL -

REVISION HISTORY

DATEBRANCHLEAD ENGRCHECKEDDRAWNDESCRIPTION REVZONE

Note 5

A

B

C

DD

C

B

A

CAGE DWG. NO. SH REV.

NATIONAL AERONAUTICS & SPACE ADMINISTRATION

LANGLEY RESEARCH CENTER

HAMPTON, VA 23681-2199

TITLE

DWG.

NO.

CAGE CODESIZE REV.

SHEETSCALE

ACT. WT.CALC. WT.

DRAWN

CHECKED

DESIGNER

LEAD ENGR

BRANCH

SPECIAL MARKING SYMSIMILAR TO

FINISH

TREATMENT

DO NOT SCALE DRAWING

APPROVALS DATE

CONTRACT NO.UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES.

TOLERANCES

DECIMALS ANGULAR

.XX .03 .X .5

.XXX .010

1 OF 11/1

-130037925305D

MEASDS PIEZO SENSOR

WELDING DETAILS

25305SENSOR_BODY_WELDING1 -

ALL SHEETS ARE REV LEVEL -

PARTS LIST

ITEM

NO.

MATERIAL

SPECIFICATION

NOMENCLATURE

OR DESCRIPTION

PART OR

IDENTIFYING NO.CAGE CODEQTY REQD

REVISION HISTORY

DATEBRANCHLEAD ENGRCHECKEDDRAWNDESCRIPTION REVZONE

Note 9

SCALE 2/1

Note:8

Note 6

Pressure Port Header

SCALE 2/1

NOTE: 7

SCALE 2/1

A

B

C

DD

C

B

A

CAGE DWG. NO. SH REV.

NATIONAL AERONAUTICS & SPACE ADMINISTRATION

LANGLEY RESEARCH CENTER

HAMPTON, VA 23681-2199

TITLE

DWG.

NO.

CAGE CODESIZE REV.

SHEETSCALE

ACT. WT.CALC. WT.

DRAWN

CHECKED

DESIGNER

LEAD ENGR

BRANCH

SPECIAL MARKING SYMSIMILAR TO

FINISH

TREATMENT

DO NOT SCALE DRAWING

APPROVALS DATE

CONTRACT NO.UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES.

TOLERANCES

DECIMALS ANGULAR

.XX .03 .X .5

.XXX .010

1 OF 11/1

-130037825305D

MEADS SUPERSONIC PRESSURE

TRANSDUCER WELDING DETAILS

25305 FINAL_WELD 1 -

ALL SHEETS ARE REV LEVEL -

REVISION HISTORY

DATEBRANCHLEAD ENGRCHECKEDDRAWNDESCRIPTION REVZONE

Mounting Hole

SCALE 3/1

Note 5 Wrench Flat

20 V2.0 9-22

SECTION 2

INSTRUCTION TO OFFERORS

☒52.212-1 Instructions to Offerors – Commercial Items (Jan 2017) Addendum to 52.212-1

Quotes for the item(s) described in the RFQ are due by 2/8/2018 by 1:00 p.m. CT to Philip M. Pearson at Philip.m.pearson@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 Philip M. Pearson at Philip.m.pearson@nasa.gov no later than 2/7/2018 by 1:00 p.m. CT. Telephone questions shall not be accepted.

The NAICS Code for this procurement is 333992.

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.

http://www.sam.gov/

21 V2.0 9-22

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

FEDERAL ACQUISITIONI REGULATION (FAR) PROVISIONS INCORPORATED BY

REFERENCE:

☒52.204-07 System for Award Management (Oct 2016) ☒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 (Oct 2015) ☐52.223-1 Biobased Product Certification (May 2012)

FAR PROVISISIONS IN FULL TEXT:

☒52.212-3 OFFEROR REPRESENTATIONS AND CERTIFICATIONS—COMMERCIAL ITEMS

(NOV 2017)

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

22 V2.0 9-22 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, 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.

23 V2.0 9-22

“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;

(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.

24 V2.0 9-22

(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

(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 --

25 V2.0 9-22

(1) That 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 stock of which is owned by one or more women; and

(2) Whose management and daily business operations are controlled by one or more women.

“Women-owned small business (WOSB) concern eligible under the WOSB Program (in accordance with 13 CFR part 127),” 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.

(b)

(1) Annual Representations and Certifications. Any changes provided by the offeror in paragraph (b)(2) of this provision do not automatically change the representations and certifications posted on the SAMwebsite.

(2) The offeror has completed the annual representations and certifications electronically via the SAM website accessed through https://www.acquisition.gov. After reviewing the SAM database information, the offeror verifies by submission of this offer that the representation and certifications currently posted electronically at FAR 52.212-3, Offeror Representations and Certifications—Commercial Items, have been entered or updated in the last 12 months, are current, accurate, complete, and applicable to this solicitation (including the business size standard applicable to the NAICS code referenced for this solicitation), as of the date of this offer and are incorporated in this offer by reference (see FAR 4.1201), except for paragraphs ____________. [Offeror to identify the applicable paragraphs at (c) through (u) of this provision that the offeror has completed for the purposes of this solicitation only, if any. These amended representation(s) and/or certification(s) are also incorporated in this offer and are current, accurate, and complete as of the date of this offer. Any changes provided by the offeror are applicable to this solicitation only, and do not result in an update to the representations and certifications posted electronically on SAM.]

(c) Offerors must complete the following representations when the resulting contract is to be performed in the United States or its outlying areas. Check all that apply.

(1) Small business concern. The offeror represents as part of its offer that it [_] is, [_] is not a small business concern.

(2) Veteran-owned small business concern. [Complete only if the offeror represented itself as a small business concern in paragraph (c)(1) of this provision.] The offeror represents as part of its offer that it [_] is, [_] is not a veteran-owned small business concern.

(3) Service-disabled veteran-owned small business concern. [Complete only if the offeror represented itself as a veteran-owned small business concern in paragraph (c)(2) of this provision.] The offeror represents as part of its offer that it [_] is, [_] is not a service-disabled veteran-owned small business concern.

(4) Small disadvantaged business concern. [Complete only if the offeror represented itself as a small business concern in paragraph (c)(1) of this provision.] The offeror represents that it [_] is, [_] is not, a small disadvantaged business concern as defined in 13 CFR 124.1002.

https://www.acquisition.gov/

26 V2.0 9-22

(5) Women-owned small business concern. [Complete only if the offeror represented itself as a small business concern in paragraph (c)(1) of this provision.] The offeror represents that it [_] is, [_] is not a women-owned small business concern.

Note: Complete paragraphs (c)(8) and (c)(9) only if this solicitation is expected to exceed the simplified acquisition threshold.

(6) WOSB concern eligible under the WOSB Program. [Complete only if the offeror represented itself as a women-owned small business concern in paragraph (c)(5) of this provision.] The offeror represents that—

(i) It [_] is, [_] is not a WOSB concern eligible under the WOSB Program, has provided all the required documents to the WOSB Repository, and no change in circumstances or adverse decisions have been issued that affects its eligibility; and

(ii) It [_] is, [_] is not a joint venture that complies with the requirements of 13 CFR part 127, and the representation in paragraph (c)(6)(i) of this provision is accurate for each WOSB concern eligible under the WOSB Program participating in the joint venture.