01903cam a2200409Ia 4500100168586MiAaHDL20250726000000.0m d cr bn ---auaua110125s1955 dcua b 000 0 eng d(MiU)990128621080106381sdr-miu.990128621080106381(MiU)MIU01000000000000012862108-goog(OCoLC)698244649(MiU)Aleph012862108CSLTEFNACARUtOrBLWNACATL589.4.C87 1955Y 3.N21/5:15/L54L06aCurfman, Howard J.Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems /by Howard J. Curfman.Washington, D.C. :National Advisory Committee for Aeronautics,1955.23 p. :ill. ;27 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierNACA research memorandum ;L54L06a"Declassified February 10, 1959.""February 15, 1955."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet.Guided missilesControl systemsAerodynamics.Guidance systems (Flight)Aerodynamics.Langley Aeronautical Laboratory.http://id.loc.gov/authorities/names/n81018841http://id.loc.gov/rwo/agents/n81018841United States.National Adviosry Committee for Aeronautics.NACA research memorandum.United States.National Advisory Committee for Aeronautics.http://id.loc.gov/authorities/names/n79060141http://id.loc.gov/rwo/agents/n79060141Technical Report Archive & Image Library (TRAIL)3901508649043310016858620241217224803.020250726000000.020260307165459.02026-03-08T12:17:53Z2026-02-22T18:30:03Z2021-03-27T20:00:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.990128621080106381MiUSDRGWLA012862108mdp.39015086490433MIU990128621080106381MIUGWLA20260308googlemdp.390150864904331955pdusncn