DEPT OF DEFENSE | DEPT OF THE ARMY has floated a tender for Gas Turbine Power System. The project location is USA and the tender is closing on 23 Jul 2025. The tender notice number is W911S225U1171, while the TOT Ref Number is 122843141. Bidders can have further information about the Tender and can request the complete Tender document by Registering on the site.

Expired Tender

Procurement Summary

Country : USA

Summary : Gas Turbine Power System

Deadline : 23 Jul 2025

Other Information

Notice Type : Tender

TOT Ref.No.: 122843141

Document Ref. No. : W911S225U1171

Financier : Self Financed

Purchaser Ownership : Public

Tender Value : Refer Document

Purchaser's Detail

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Tender Details

Description

A complete gas-turbine power system to consist of an engine designed and manufactured for engineering education. Engine must utilize a centrifugal flow compressor, reverse flow annular combustor and an axial flow turbine stage. Engine to be of current manufacture and consisting of all new components. All engine components either vacuum investment cast or precision CNC machined. All high-heat components manufactured from 17-4 ph stainless steel, Inconel- 718 or CMR 247 Super Alloy. Traceable and verifiable material to be used throughout engine. All elements comprising the system to be contained in a rigid steel chassis mounted on rolling castors. All system metal surfaces to be stainless steel, anodized or powder coated to promote durability and wear resistance. Complete system not to require any permanent facility modifications or additions, self-contained. Engine situated behind transparent protective shields allowing clear view during operation. Operator capable of manual control throughout entire range of operation. Operator panel to consist of digital TIT, EGT, and RPM indicators, analog oil pressure, engine pressure ratio, fuel pressure and air pressure gauges, keyed master, green start, red stop and T-handled power control lever. System to be equipped with calibrated transducers and thermocouples capable of measuring compressor inlet, compressor exit, turbine stage inlet, turbine stage exit and thrust nozzle exit temperature and pressures, fuel flow, thrust and engine compressor / turbine rotational speed. Engine thrust to be measured by a load cell permitting direct indication of thrust value. To be supplied with a USB based digital data LabView acquisition system complete with computer and user configurable LabView data acquisition software capable of measuring and recording analog, digital and frequency signals. Fully automatic engine start and operational health monitoring system provided with LCD status readout and cumulative run- time and...
Active Contract Opportunity
Notice ID : W911S225U1171
Related Notice
Department/Ind. Agency : DEPT OF DEFENSE
Sub-tier : DEPT OF THE ARMY
Major Command : AMC
Sub Command : ACC
Sub Command 2 : MISSION INSTALLATION CONTRACTING COMMAND
Sub Command 3 : 419TH CSB
Office : W6QM MICC-FT DRUM
General Information
Contract Opportunity Type: Combined Synopsis/Solicitation (Original)
Original Published Date: Jul 16, 2025 02:34 pm EDT
Original Date Offers Due: Jul 23, 2025 07:15 am EDT
Inactive Policy: Manual
Original Inactive Date: Jul 16, 2026
Initiative: None

Classification
Original Set Aside: Total Small Business Set-Aside (FAR 19.5)
Product Service Code: 2835 - GAS TURBINES AND JET ENGINES; NON-AIRCRAFT PRIME MOVER, AIRCRAFT NON-PRIME MOVER, AND COMPONENTS
NAICS Code: 333618 - Other Engine Equipment Manufacturing

Place of Performance: 10996

Documents

 Tender Notice


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