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This Combined Synopsis/Solicitation opportunity from Department Of Defense was posted on July 16, 2025. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

Gas Turbine Power System

Closed
W911S225U1171Federal

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NAICS: 333618
New
DIBBS
SENSOR, EXHAUST GAS, OXY
Solicitation # SPE7L5-27-T-0429
This fixed-price solicitation, issued by the Defense Logistics Agency (DLA) Weapons Support Land Supplier Operations Engines, is for the procurement of six units of exhaust gas oxygen emission control sensors, identified by NSN 2990-01-697-7963. These sensors are designated as critical application items and must conform to TDP Rev A Gen 3 and Basic Drawing NR 53711 8599721. The delivery period is 147 days after receipt of order, with a need ship date of April 6, 2027, and delivery to the DLA Distribution DDSP New Cumberland facility in Pennsylvania. Inspection and acceptance will occur at the destination. The contract imposes rigorous technical and quality standards, including compliance with DLA Master List requirements (RA001), tailored higher-level quality requirements (RQ001), and configuration change management (RQ002). Packaging and marking must adhere to MIL-STD-2073-1E and MIL-STD-129, with palletization following RP001. Due to the nature of the technical data, the contract is subject to ITAR and EAR export controls, requiring approved US/Canada Joint Certification Program certification. Additionally, the contractor must comply with CMMC Level 2 certification, DFARS safeguarding of covered defense information, and specific mercury containment standards per NAVSEA 5100-003D. Invoicing must be processed electronically through the Wide Area WorkFlow (WAWF) system.
DLA WEAPONS SUPPORT LAND SUPPLIER OPNS ENGINES

POSTED

about 15 hours ago

DEADLINE

in 11 days

AI Contract Overview

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This contract involves the procurement of a complete gas-turbine power system designed specifically for engineering education. The system features a high-performance engine with a single-stage centrifugal compressor, a reverse flow annular combustor, and an axial flow turbine stage, all constructed from new, traceable materials such as 17-4 PH stainless steel, Inconel 718, or CMR 247 Super Alloy. The engine components are precision CNC machined or vacuum investment cast, ensuring durability and reliability. The entire system is housed in a sturdy steel chassis mounted on rolling castors, with metal surfaces treated for wear resistance, and is fully self-contained, requiring no permanent modifications to the facility. It includes transparent shields for safe operation, manual control capabilities, and a comprehensive operator panel with digital and analog gauges, along with safety and operational instructions. The system is equipped with advanced sensors, thermocouples, and a digital data acquisition system powered by LabView software, enabling detailed measurement of temperatures, pressures, fuel flow, thrust, and rotational speeds. Thrust is directly measured via a load cell, and the system features automatic start-up and health monitoring with status displays. It supports multiple approved fuels, including Jet A, B, JP-4, and diesel, and operates at a maximum thrust of 40 lbf with a maximum RPM of 87,000. The contract is issued by the Department of the Army under a small business set-aside, with a response deadline of July 23, 2025. It guarantees spares availability, technical support, and comprehensive documentation, ensuring the system's suitability for educational and training purposes.

General Info

Delivery of a gas turbine training system with advanced alloys, sensors, data acquisition, and full support.

NAICS

333618 - Other Engine Equipment Manufacturing

Place of Performance

NY, 10996

Set-Aside

SBA

Documents

1

W911S225U1171_S2P2_Brand_Name_or_Equal_Boss__Michael_J_CIV_USARMY_USMA__USA__2025_07_16_140858__EST_.pdf

PDF

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Timeline

PhaseClosed
Posted

Combined Synopsis

Response Deadline

Deadline has passed

Submission Closed

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Organization & Contact Information

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AgencyDepartment Of Defense → W6QM Micc-Ft Drum
Contacts2 people available
OfficeFORT DRUM, NY, 13602-5220, USA
Office AddressFORT DRUM, NY, 13602-5220, USA

Full Description

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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 cycle count. Representative engine components and technical data optionally available for teaching use and training aids. Manufacturer to guarantee spares availability and provide technical support services for core engine and power system. Provided with a comprehensive Operator?s Manual. Provided with summary operating checklist for all operating conditions. Provided with safety instruction to address all operating conditions. Power:120V single-phase 60Hz. Design Maximum Thrust: 40 lbf (178 N). Approved Fuels: Jet A,A-1, B; JP-4, 5, 8; Kerosene, Diesel, Fuel Oil #1 or #2. Compressor Type: Single Stage Centrifugal (Radial Outflow). Approved Oils: MIL-PRF-23699F-STD, Sensors(Preinstalled and Calibrated) Compressor Inlet Temperature and Pressure (T1/P1) Compressor Exit Temperature and Pressure (T02/P02). Turbine Stage Inlet Temperature and Pressure (T03/P3) Turbine Stage Exit Temperature and Pressure (T04/P04). Thrust Nozzle Exit Temperature and Pressure (T05/P05). Fuel Flow Thrust Engine Rotational Speed (RPM). Digital Turbine Inlet Temperature (TIT). Digital Exhaust Gas Temperature (EGT). Digital Engine Rotational Speed (RPM). Analog Oil Pressure. Analog Engine Pressure. Analog Air Start Pressure. Design Maximum RPM: 87,000. Engine Compression Ratio: 3.4, Engine Pressure Ratio: 30.0. Exhaust Gas Temperature: 1328 - F (720 - C)

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