Fiscal Year 2016 SBIR/STTR Appendices 7 System A high fidelity Prototype software exists Documented prototype engineering unit that having all key functionality test adequately addresses available for performance in an all critical scaling demonstration and test. demonstrating operational issues is built and Well integrated with agreement environment. operated in a relevant operational with analytical environment to hardware/software predictions. demonstrate systems demonstrating performance in the operational feasibility. actual operational Most software bugs environment and removed. Limited platform (ground, documentation available. airborne, or space). 8 Actual The final product in its All software has been Documented system final configuration is thoroughly debugged and test completed successfully fully integrated with all performance and "flight demonstrated through operational hardware and verifying qualified" test and analysis for its software systems. All user analytical through test intended operational documentation, training predictions. and environment and documentation, and platform (ground, maintenance airborne, or space). documentation completed. All functionality successfully demonstrated in simulated operational scenarios. Verification and Validation (V&V) completed. 9 Actual The final product is All software has been Documented system flight successfully thoroughly debugged and mission proven operated in an integrated with all operational through actual mission. operational results. successful hardware/software mission systems. All operations. documentation has been completed. Sustaining software engineering support is in place. System has been successfully operated in the operational environment.
Fiscal Year 2016 SBIR/STTR Appendices 7 System prototype in an operational environment. A high fidelity engineering unit that adequately addresses all critical scaling issues is built and operated in a relevant environment to demonstrate performance in the actual operational environment and platform (ground, airborne, or space). Prototype software exists having all key functionality available for demonstration and test. Well integrated with operational hardware/software systems demonstrating operational feasibility. Most software bugs removed. Limited documentation available. Documented test performance demonstrating agreement with analytical predictions. 8 Actual system completed and "flight qualified" through test and The final product in its final configuration is successfully demonstrated through test and analysis for its intended operational environment and platform (ground, airborne, or space). All software has been thoroughly debugged and fully integrated with all operational hardware and software systems. All user documentation, training documentation, and maintenance documentation completed. All functionality successfully demonstrated in simulated operational scenarios. Verification and Validation (V&V) completed. Documented test performance verifying analytical predictions. 9 Actual system flight proven through successful mission operations. The final product is successfully operated in an actual mission. All software has been thoroughly debugged and integrated with all operational hardware/software systems. All documentation has been completed. Sustaining software engineering support is in place. System has been successfully operated in the operational environment. Documented mission operational results.
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