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- W2029047943 abstract "Flight testing of the Space Shuttle Orbiter is in progress and current results of the post-flight aerodynamic analyses are discussed. The purpose of these analyses is to reduce the pre-flight aerodynamic uncertainties, thereby leading to operational certification of the Orbiter flight envelope relative to the integrated airframe and flight control system. Primary data reduction is accomplished with a well documented maximum likelihood system identification techniques." @default.
- W2029047943 created "2016-06-24" @default.
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- W2029047943 date "1982-08-09" @default.
- W2029047943 modified "2023-09-27" @default.
- W2029047943 title "Stability and control flight test results of the space transportation system's orbiter" @default.
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- W2029047943 doi "https://doi.org/10.2514/6.1982-1316" @default.
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