SATPC0042252 Tab 04 4 SOW..pdf

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Attached to
MTS FlexTest 40 Controller Federal contract opportunity
Solicitation number
80NSSC26940125Q
Issued by
National Aeronautics and Space Administration Shared Services Center

About this file

This is a Statement of Work for the acquisition of MTS FlexTest 40 Controllers for NASA Langley Research Center (LaRC) located at 4 S Marvin St, Hampton, VA 23681. The requirement specifies the procurement of two MTS FlexTest 40 Controller units, each configured with identical components including two Eight Channel Analog Input Boards (Model 494.45) per unit. The scope includes numerous cable assemblies and related components with specific technical specifications: two dual series 252 servovalve cable assemblies (7.5 m each), six series 252 and 256 valve cable assemblies to Model 494.16 (7.5 m each), four load cell cable assemblies with various connector types (RJ50 to MS, RJ50 to PC, totaling 7.5 m each), six load cell cables with RJ50 to PT connectors (7.5 m each), eight LVDT cable assemblies with RJ50 to PT connectors (7.5 m each), four service manifold cable assemblies (two Off/Low/High 24V DC models, two Model 298.11 On/Off 24V DC models, all 7.5 m), and four proportional valve D9 to MS connector service manifold cable assemblies (7.5 m each).

The period of performance is 95 days after receipt of order (ARO). No pricing information, response dates, award dates, or other contractual terms are specified in this document, as it focuses solely on defining the technical requirements and specifications for the equipment and components to be delivered to the NASA facility in Hampton, Virginia.

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SATPC0042252 Tab 06 RDSS..pdf PDF
SATPC0042252 Tab 07 Capability Statement.pdf PDF

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Text version

STATEMENT OF WORK

1. Objective/Requirements

This requirement is for the acquisition of the MTS FlexTest 40 Controllers for NASA

Langley Research Center (LaRC). The information listed below is required to complete this purchase.

2. Characteristics, Scope, and Specs

QTY DESCRIPTION

2 MTS FlexTest 40 Controller with the following configuration:

1 Eight Channel Analog Input Board; Model 494.45

1 Eight Channel Analog Input Board; Model 494.45

1 Cable Assembly; Dual Series 252 Servovalve, out of phase, 7.5 m (25 ft)

1 Cable Assembly; Dual Series 252 Servovalve, out of phase, 7.5 m (25 ft)

3 Cable Assembly; Series 252 and Series 256 valves to Model 494.16, 7.5 m

(25 ft)

3 Cable Assembly; Series 252 and Series 256 valves to Model 494.16, 7.5 m

(25 ft)

1 Cable Assembly; Load Cell with RJ50 to MS connector, 7.5 m (25 ft)

1 Cable Assembly; Load Cell with RJ50 to MS connector, 7.5 m (25 ft)

1 Cable Assembly; Load Cell with RJ50 to PC connector, 7.5 m (25 ft)

1 Cable Assembly; Load Cell with RJ50 to PC connector, 7.5 m (25 ft)

3 Load Cell Cable; RJ50 to PT, 7.5 m (25 ft)

3 Load Cell Cable; RJ50 to PT, 7.5 m (25 ft)

4 LVDT Cable Assembly; RJ50 to PT, 7.5m (25ft)

4 LVDT Cable Assembly; RJ50 to PT, 7.5m (25ft)

1 Cable Assembly; Service Manifold, Off/Low/High, 24 V DC, 7.5 m (25 ft)

1 Cable Assembly; Service Manifold, Off/Low/High, 24 V DC, 7.5 m (25 ft)

1 Cable Assembly; Model 298.11 Service Manifold, On/Off, 24 V DC, 7.5 m

(25 ft)

1 Cable Assembly; Model 298.11 Service Manifold, On/Off, 24 V DC, 7.5 m

(25 ft)

2 Cable Assembly; Service Manifold, proportional valve D9 to MS connector,

7.5 m (25 ft)

2 Cable Assembly; Service Manifold, proportional valve D9 to MS connector,

7.5 m (25 ft)

3. Place of Performance

NASA Langley Research Center

4 S Marvin St

Hampton, VA 23681

4. Period of Performance

95 days ARO

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