During the arctic test phase of the F-111D DT/E All-Weather Test Program, 24.0 hours of test time were accumulated in 12 test flights. Five of these flights were selected as being most representative of aircraft operation in an arctic environment. All available data obtained on these five flights are presented in this document as computer printouts.
F-111D, DT and E Evaluation of Environmental Control, Airframe, Flight Control, and Secondary Power Subsystems. Appendix I
1973
485 pages
Report
Keine Angabe
Englisch
Aircraft , Jet fighters , Flight testing , Fighter bombers , Cold weather tests , Arctic regions , Environmental tests , Deicing systems , Avionics , Heating , Cooling and ventilating equipment , Cockpits , Temperature , Flight control systems , Airframes , Hydraulic equipment , Data processing , Computer printouts , Checkout procedures , Performance(Engineering) , F-111 aircraft , F-111D aircraft
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