01710oam 2200493 450 991070623960332120171023100139.0(CKB)5470000002456043(OCoLC)858246018(EXLCZ)99547000000245604320130912j200003 uh 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierOptimal pitch thrust-vector angle and benefits for all flight regimes /Glenn B. Gilyard, Alexander BolonkinEdwards, California :National Aeronautics and Space Administration, Dryden Flight Research Center,March 2000.1 online resource (22 pages) illustrationsNASA/TM ;2000-209021"March 2000.""Performing organization: NASA Dryden Flight Research Center"--Report documentation page.Includes bibliographical references (page 22).Pitch (inclination)nasatThrust vector controlnasatAutomatic flight controlnasatAngles (geometry)nasatPitch (inclination)Thrust vector control.Automatic flight control.Angles (geometry)Gilyard Glenn B.1393171Bolonkin AlexanderHugh L. Dryden Flight Research Center,OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706239603321Optimal pitch thrust-vector angle and benefits for all flight regimes3454920UNINA