Performance and stability and control testing was conducted on a production model OV-1D airplane (Mohawk), S/N 68-16990, to evaluate its ability to perform the manned aerial surveillance mission and to determine military specification compliance. Nine flights were accomplished for a total of 20.5 hours. The stability and control portion of the testing is presented in this report. The performance test results will be contained in an addendum.
Army Preliminary Evaluation II Production OV-1D (Mohawk) Performance and Handling Qualities
1971
61 pages
Report
Keine Angabe
Englisch
Aircraft , Observation aircraft , Flight testing , Performance(Engineering) , Aerodynamic characteristics , Quality control , Cockpits , Human factors engineering , Instrument panels , Taxiing , Takeoff , External stores , Radar equipment , Short takeoff aircraft , Stability , Yaw , Pitch(Motion) , Maneuverability , Stalling , Airspeed , Ov-1 aircraft , Ov-1d aircraft , V-1 aircraft
Army Preliminary Evaluation Preproduction OV-1D (Mohawk)
NTIS | 1970
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