Go to DI-SESS-82321 at DAPS Quick Search ASSIST<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"The Air Vehicle Flight Performance Description Report for Rotorcraft and Propeller-driven Fixed-wing Aircraft provides engineering design, test and analysis information quantifying the flight performance characteristics, capabilities and limitations of air vehicles. The information contained in the report and supporting documentation will be used to support development of a flight performance model of the air vehicle. This model will be used to calculate performance characteristics and mission capabilities throughout the flight envelope. The data provided will also be used to calibrate conceptual design tools for future acquisition programs and design trade studies. It is the purpose of this Data Item Description (DID) to ensure complete documentation of the air vehicle flight performance at a level of data quality and substantiation consistent with the current design stage of the air vehicle.<\/p>\n","protected":false},"featured_media":0,"template":"","categories":[3244],"tags":[],"sdo":[1337],"topic":[],"fsc":[3566],"document_type":[3246],"class_list":["post-201915","mil-spec","type-mil-spec","status-publish","hentry","category-data-item-description","sdo-us-dod","fsc-sess","document_type-data-item-description"],"acf":[],"yoast_head":"\n
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The information contained in the report and supporting documentation will be used to support development of a flight performance model of the air vehicle. This model will be used to calculate performance characteristics and mission capabilities throughout the flight envelope. The data provided will also be used to calibrate conceptual design tools for future acquisition programs and design trade studies. 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