Estimation of Range of Stability Derivatives for Current and Future Pilotless Aircraft
Description:
Memorandum presenting an analysis made of the probable range of the stability parameters of present and future missiles. Included is a short review of the dynamic theory and some of the factors and assumptions influencing the stability derivatives and equations of motion.
Date:
October 8, 1947
Creator:
Pitkin, Marvin & Ankenbruck, Herman O.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department