000			02100nam a22002897a 4500
003			OSt
005			20220715120655.0
008			220715b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administration
245			_aNasa technical note [NASA TN D 1921-1930]
260			_aWashington, D.C. _bNational Aeronautics and Space Administration _c1963
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical Note
500			_aNASA TN D-1921: Handling qualities and trajectory requirements for terminal lunar handling as determinated from analog simulation by Gene J. Matranga 33p
500			_aNASA TN D-1922: Flight test of a pitch control for a spinning vehicle by H. D. Garner 13p
500			_aNASA TN D-1923: Study of a guidance scheme using approximate solutions of trajectory equations to control the aerodynamics skip flight of a reentry vehicle by Robert S. Dunning 33p
500			_aNASA TN D-1924: Rough air effect on crew performance during a simulated low altitude high speed survelliance mission by George J. Hurt 22p
500			_aNASA Tn D-1925: An analysis of VG and VGH operational data from a twin engine turboprop transport airplane by Paul A. Hunter 45p
500			_aNASA TN D-1926: Transonic investigation of the effects of nose bluntness fineness ratio cone angle and base shape on the static aerodynamic characteristics of short blunt cones at angles of attack to 180 degree by Cuyler W. Brooks 39p
500			_aNASA TN D-1928: Arrest of a moving mass by an attached membrane by Manual Stein 13p
500			_aNASA TN D-1929: Static aerodynamic charectristics of three rocket vehicle configurations at mach numbers from 1.80 to 4.63 including some effects of fin size fin cant and auxiliary rocket motors by Dennis E. Fuller 51p
500			_aNASA TN D-1930: Aerodynamic loading charectristics of a 1/10 scale model of the three stage scout vehicle at mach numbers from 1.57 to 4.65 by Lloyd S. Jernell 36p
650			_aThermal
942			_cTR
999			_c565898 _d565898