Technology_Readiness_Levels_Defined.pdf

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Attached to
Arm/Disarm Switch Replacement (ADSR) Program Federal contract opportunity
Solicitation number
FA8214-19-R-7003
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

About this file

This document contains a federal contract solicitation and supporting technical documentation. The solicitation is for an Arm/Disarm Switch Replacement program to provide a fit and function replacement switch for the Minute Man III weapon system. The replacement switch must maintain backwards compatibility. The contract will have an initial multiple award IDIQ structure with task orders awarded. The first task order is for development and qualification activities, with preliminary design review required within 10 weeks of award. Production units are due 12 months after award with qualification testing completed within 18 months. Future production delivery orders will be competed only among qualified designs. The intent is to procure enough switches to meet supply needs through December 2029. Participation may be restricted to Ensign-Bickford Aerospace & Defense Company, Moog Space and Defense Group, and Bionetics based on ability to meet schedule. The supporting technical documentation defines technology readiness levels and provides descriptions and examples to support each level.

TRL Level Def.

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Other files for this federal contract opportunity

Other files attached to Arm/Disarm Switch Replacement (ADSR) Program, newest first.
File Type Posted
FA821419R7003_v2.pdf PDF
Intro_Letter.docx DOCX document
FA821419R7003.pdf PDF
ADSR_SOO.pdf PDF
ADSR_GRID.pdf PDF
ADSR_Contractor_Down_Select_Criteria.pdf PDF
ADSR_CDRL_Package.pdf PDF
ADSR_WBS.xlsx XLSX spreadsheet
Synopses.docx DOCX document

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2-13

2.5 TRL Definitions, Descriptions, and Supporting Information

TRL Definition Description Supporting Information 1 Basic principles observed and reported.

Lowest level of technology readiness. Scientific research begins to be translated into applied research and development (R&D). Examples might include paper studies of a technology’s basic properties.

Published research that identifies the principles that underlie this technology.

References to who, where, when.

2 Technology con-cept and/or appli-cation formulated.

Invention begins. Once basic principles are observed, practical applica-tions can be invented. Appli-cations are speculative, and there may be no proof or detailed analysis to support the assumptions. Examples are limited to analytic studies.

Publications or other references that out-line the application being considered and that provide analysis to support the concept.

3 Analytical and experimental criti-cal function and/or characteristic proof of concept.

Active R&D is initiated. This includes analytical studies and laboratory studies to physically validate the analytical predictions of separate elements of the technology. Examples include components that are not yet integrated or representative.

Results of laboratory tests performed to measure parameters of interest and com-parison to analytical predictions for critical subsystems. References to who, where, and when these tests and comparisons were performed.

4 Component and/or breadboard valida-tion in a laboratory environment.

Basic technological compo-nents are integrated to establish that they will work together. This is relatively “low fidelity” compared with the eventual system. Exam-ples include integration of “ad hoc” hardware in the laboratory.

System concepts that have been consi-dered and results from testing laboratory-scale breadboard(s). References to who did this work and when. Provide an esti-mate of how breadboard hardware and test results differ from the expected sys-tem goals.

5 Component and/or breadboard valida-tion in a relevant environment.

Fidelity of breadboard technology increases significantly. The basic technological components are integrated with reasonably realistic supporting elements so they can be tested in a simulated environment. Examples include “high-fidelity” laboratory integration of components.

Results from testing laboratory breadboard system are integrated with other supporting elements in a simulated operational environment. How does the “relevant environment” differ from the expected operational environment? How do the test results compare with expectations? What problems, if any, were encountered? Was the breadboard system refined to more nearly match the expected system goals?

6 System/subsystem model or prototype demonstration in a relevant environment.

Representative model or prototype system, which is well beyond that of TRL 5, is tested in a relevant environ-ment. Represents a major step up in a technology’s demonstrated readiness.

Examples include testing a prototype in a high-fidelity

Results from laboratory testing of a proto-type system that is near the desired con-figuration in terms of performance, weight, and volume. How did the test environment differ from the operational environment?

Who performed the tests? How did the test compare with expectations? What problems, if any, were encountered?

What are/were the plans, options, or

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TRL Definitions, Descriptions, and Supporting Information (Continued)

TRL Definition Description Supporting Information laboratory environment or in a simulated operational environment.

actions to resolve problems before moving to the next level?

7 System prototype demonstration in an operational environment.

Prototype near or at planned operational system. Repre-sents a major step up from TRL 6 by requiring demon-stration of an actual system prototype in an operational environment (e.g., in an air-craft, in a vehicle, or in space).

Results from testing a prototype system in an operational environment. Who per-formed the tests? How did the test com-pare with expectations? What problems, if any, were encountered? What are/were the plans, options, or actions to resolve problems before moving to the next level?

8 Actual system completed and qualified through test and demonstration.

Technology has been proven to work in its final form and under expected conditions. In almost all cases, this TRL represents the end of true system development. Examples include developmental test and evaluation (DT&E) of the system in its intended weapon system to deter-mine if it meets design specifications.

Results of testing the system in its final configuration under the expected range of environmental conditions in which it will be expected to operate. Assessment of whether it will meet its operational requirements. What problems, if any, were encountered? What are/were the plans, options, or actions to resolve problems before finalizing the design?

9 Actual system proven through successful mission operations.

Actual application of the technology in its final form and under mission condi-tions, such as those encountered in operational test and evaluation (OT&E).

Examples include using the system under operational mission conditions.

OT&E reports.

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