Product Description_V250 and T408 TMS Kit.pdf
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- Attached to
- V250 AND TMS KIT
- Solicitation number
- W58RGZ25P0016
About this file
This Product Description document outlines a requirement by the Prototype Integration Facility (PIF) at Combat Capabilities Development Command (DEVCOM) Aviation and Missile Center, Redstone Arsenal, Alabama, to procure a Torque Measurement System (TMS) for the V250 and T408 aircraft engine testing. The solicitation requires two primary deliverables: a V250/T408 Torque Measurement System Kit and a V250 Application Study for the T408 Aircraft Engine.
The TMS Kit must include a module with shaft-to-engine components, plumbing, calibration kit with weights, and electronics (signal processor, Rotastat Control, and 90 ft. cable). The application study requires the contractor to evaluate the V250 Dynamometer for T408 Turboshaft Engine testing, defining interface requirements, considering test plans, inertia, speeds, and power. Deliverables include special rotor considerations, identifying torque measurement equipment, and potential updates to drawings and documents. The document is dated 26 June 2025 and is associated with Solicitation Number W58RGZ25P0016, with a response deadline of 10 July 2025.
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| File | Type | Posted |
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| Sources Sought_V250 and T408 TMS Kit.docx | DOCX document |
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Text version
26 June 2025
PRODUCT DESCRIPTION
The Prototype Integration Facility (PIF), Combat Capabilities Development Command (DEVCOM) Aviation and Missile Center, Redstone Arsenal, Alabama, has a requirement to procure a Torque Measurement System to interoperate with a Variable-Geometry, Radial Outflow Compressor (VAROC) Air Dynamometer 250 and T408 aircraft engine in support of Flexible Engine Diagnostics Systems (FEDS).
Description of Required Supplies/Services:
Description
V250 / T408 Torque Measurement System Kit
The contractor shall provide the following with the TMS Kits:
- TMS Module / Shaft to engine components: spline adapter and splined hub, if necessary.
- TMS Plumbing
- TMS Calibration Kit with weights
- Electronics: Signal processor, Rotastat Control and 90 ft. cable
V250 Application Study for the T408 Aircraft Engine
The contractor shall evaluate the V250 Dynamometer with respect to testing objectives and configuration needs for testing the GE T408 Turboshaft Engine. The contractor shall define the specific interphase requirements with consideration to test plans, including inertia requirements, speeds, and power.
The following are deliverables as a result of this application study:
- Special Rotor consideration for inertia requirements
- Identifying the torque measurement equipment, including but not limited to torque meter, interconnect shafts, and electronics.
- Upon determining appropriate torque meter system, CN will update or generate new drawings and documents and enable life solutions.
File details come from the government source that posted it. Updated .