The document presents an overview of the five Laboratory Thrusts extracted from the FY 84 Research and Technology Plan of the Flight Dynamics Laboratory omitting specific funding and timing information of an 'Official Use Only' nature. Technical objectives are described for the thrusts of Tactical Force Multiplier, Runway Independence, Space and Missile Applications, Strategic Aeronautical Applications, and Multimission Core Technology.
Air Force Technical Objective Document, Air Force Wright Aeronautical Laboratories, Flight Dynamics Laboratory, Fiscal Year 1984
1982
54 pages
Report
Keine Angabe
Englisch
Research Program Administration & Technology Transfer , Technology forecasting , Defense planning , Air Force planning , Aircraft , Spacecraft , Aerodynamics , Aeronautical laboratories , Aerodynamic characteristics , Aerodynamic configurations , Aerodynamic control surfaces , Aerodynamic heating , Cost effectiveness , Combat effectiveness , Runways , Vulnerability , Space technology , Guided missiles , Penetration , Bomber aircraft