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Here’s a GSA description of this SIN#.  Following is a list of Projects we have worked on relating to this SIN #

Services required under this SIN involve the application of various techniques demonstrating that a prototype system (subsystem, program, project or activity) performs in accordance with the objectives outlined in the original design.  Typical associated tasks include, but are not limited testing of a prototype and first article(s) testing, environmental testing, independent verification and validation, reverse engineering, simulation and modeling (to test the feasibility of a concept), system safety, quality assurance, physical testing of the product or system, training, privatization and outsourcing.

Example:  The navigation satellite-working model will be subjected to a series of tests, which may simulate and ultimately duplicate its operational environment.

Architect-Engineering (A/E) Services as that term is defined in FAR 36.601-3 are excluded from the PES Schedule. If the agency’s statement of work, substantially or to a dominant extent, specifies performance or approval by a registered of licensed architect or engineer for services related to real property, the Brooks Architect-Engineers Act applies and such services must be procured in accordance with FAR Part 36.  Use of this schedule for Brooks Act architectural or engineering services is not authorized. Inappropriate use of this SIN is providing professional engineering services not specifically related to testing and evaluating and associated disciplines.

Project 1: Advanced Aircraft Simulator Flight Fidelity Evaluation Measures - Develop new methodology to evaluate the fidelity of flight simulators that relies completely on quantitative measures.

Project 2: Handling Qualities Specification Requirements for Maritime Rotorcraft, VTOL UAV, and Heavy Lift Helicopters - Developing an aeronautical design standard and simulation toolbox to address the urgent needs of rotorcraft, heavy lift helicopter, and VTOL UAV handling qualities requirements for shipboard operations.

Project 3: Enhanced Rotorcraft Aerodynamic Modules to Support Flight Testing

Developed advanced rotorcraft aerodynamic modules to significantly enhance and improve the analytical prediction of rotorcraft performance, flying quality, and loads in support of vehicle design, manufacturing, operation, and flight testing.

Project 4: Enhanced Rotorcraft Aerodynamic Modules to Support Flight Testing

Develop computationally scalable software to utilize massively parallel computer systems to efficiently predict performance and stability in support of flight testing.

Advanced Rotorcraft Technology, Inc.

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