Curtiss-Wright Overhead Module

SPEC SHEET/ STATEMENT OF WORK 1. Objective/Requirements The effort for the flight instrumentation system is 3-fold for the GoSWIFT project under FDC. 1) Establish a flight instrumentation system capability for the F15D flight test pod. 2) Instrument the Flight test pod for specific GoSWIFT requirements. 3) Update F15D 884 instrumentation system as we see fit for continual usage up to about a decade. Stack #1: This is a Spare+Upgrade overhead module stack for the existing Nose Data Acquisition Unit. Stack #2: This is a Spare+Upgrade overhead module stack for the existing Ammo Bay Data Acquisition Unit. Stack #3: This is a new mini-stack specifically chosen to provide real time 1553 data to the GoSWIFT experiment to maintain proper data time correlation. Stack #4: This is a full data acquisition unit stack chosen to provide all data measurement requirements within the flight test pod as well as cover all GoSWIFT measurement requirements. Spares: These are individual data acquisition module spares picked to provide immediate spare capabilities for Stack #4. No alternates approved. NASA Quality Document Q1-A compliance required (I.E. FAA 8130, manufactures Certificate of Conformance or OEM trace.) Q-2 Test reports, etc. 2. Characteristics, Scope, and Specs -- 1 of 5 -- -- 2 of 5 -- -- 3 of 5 -- -- 4 of 5 -- 3. Place of Performance or Delivery Location NASA Armstrong Flight Research Center Bldg 4876 Warehouse #6, Lilly Drive Edwards, CA 93524 4. Period of Performance or delivery date/need by date required Needed not later than 3/1/2027 Warranty requirements? Standard manufacturer’s warranty OK. Warranty may be broken when we conduct workmanship inspection. Broker import requirements, if applicable. N/A Freight Delivery requirements, if applicable. – N/A *If FREIGHT shipment is required, it needs to be coordinated 4 business days in advance to ensure the delivery driver has proper entry into Edwards Air Force Base. An AFRC visitor request may need to be submitted. -- 5 of 5 --