SATPC0041456 Tab 04 4 SOW.pdf

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Purchase of TOOLING FOR MITSUBISHI MD+PRO II WIRE EDM
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80NSSC26936035Q
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This is a Statement of Work for the procurement of tooling and accessories for a Mitsubishi MD+Pro II Wire EDM machine (Model BA8, Serial Number 50DB8327) located at NASA Ames Research Center's Instrument Development Laboratory.

NASA Ames requires System 3R-compatible tooling to expand fabrication capability, improve setup repeatability, and maximize operational efficiency. The specified tooling components, all manufactured by System 3R, include: two Reference Elements (298 mm/M8-50), one 3Ruler (365 x 45 x 30 with clamps and Z-Line supports), one User Kit for WEDM, one Super Vice (0–150 mm Magnum), one WEDM Presetting Station (12 x 8 x 4), one Manual Lathe Chuck (Macro), and one 3R Taper Hardinge 5C Macro Adapter (T7535). All tooling must be fully compatible with existing System 3R infrastructure currently installed on the machine, delivered complete and fully assembled, and consist of new components free from defects. The procurement period of performance is 30 days or less from Award and Requisition Order (ARO). The NASA Technical Point of Contact is Emmett Quigley, NASA Ames Research Center, Mailstop 245-6, Moffett Field, CA 94035.

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SATPC0041456 Tab 10 Open Market RFQ.pdf PDF
SATPC0041456 Tab 10 BNJ Redacted.pdf PDF

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STATEMENT OF WORK

TOOLING FOR MITSUBISHI MD+PRO II WIRE EDM

MODEL: BA8 SERIAL NUMBER: 50DB8327

1. Background

The Mitsubishi MD+Pro II Wire EDM machine is utilized in the fabrication of precision tooling and flight-quality hardware supporting laboratory astrophysics, astrochemistry, astrobiology instrumentation, and small satellite development projects within the Ames Instrument Development Laboratory.

The existing tooling package associated with this machine was supplied as part of the Original Equipment Manufacturer (OEM) configuration and has provided reliable service.

However, additional and upgraded tooling is required to support current metrological, tolerancing, repeatability, and work-holding requirements associated with modern scientific and aerospace hardware fabrication.

The existing work-holding platform is based on the System 3R tooling philosophy and interface standard. Maintaining compatibility with the installed System 3R infrastructure is necessary to preserve tooling interchangeability, setup repeatability, operator familiarity, and process consistency across ongoing laboratory operations.

Improved work-holding capability and presetting functionality will reduce setup time, minimize operator intervention, improve machining efficiency, and support more predictable delivery schedules for mission-critical hardware.

2. Scope

NASA Ames Research Center currently operates a Mitsubishi MD+Pro II Wire EDM machine equipped with System 3R-compatible work-holding components.

NASA Ames Research Center requires the procurement of additional System 3R-compatible tooling and accessories to expand fabrication capability, improve setup repeatability, and maximize operational efficiency within the Ames Instrument Development Laboratory.

3. Specifications

The Government has a requirement for tooling compatible with the Mitsubishi MD+Pro II Wire EDM machine and existing System 3R tooling infrastructure.

The required tooling, manufactured by System 3R, includes the following:

• Reference Element 298 mm/M8-50 (Qty: 2)

• 3Ruler 365 x 45 x 30 with clamps, Z-Line supports, and associated hardware (Qty: 1)

• User Kit, WEDM (Qty: 1)

• Super Vice, 0–150 mm Magnum (Qty: 1)

• WEDM Presetting Station, 12 x 8 x 4 (Qty: 1)

• Manual Lathe Chuck, Macro (Qty: 1)

• 3R Taper Hardinge 5C Macro Adapter, T7535 (Qty: 1)

4. Compatibility Requirement

All tooling supplied under this procurement shall be fully compatible with existing System 3R tooling, pallets, references, and interfaces currently installed and operational on the Mitsubishi MD+Pro II Wire EDM system at NASA Ames Research Center.

No substitute tooling systems shall be accepted that require modification of existing infrastructure, adapters, machine interfaces, or operating procedures.

5. Delivery Requirements

All tooling shall be delivered complete, fully assembled where applicable, and ready for installation and operational use upon receipt.

All supplied components shall be new and free from defects

6. Period of Performance: 30 days or less from ARO

NASA Technical POC:

Emmett Quigley NASA Ames Research Center Mailstop 245-6 Moffett Field, CA 94035

File details come from the government source that posted it. Updated .