Nasa technical note [NASA TN D 1921-1930]
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.- Washington, D.C.: National Aeronautics and Space Administration, 1963
.- ( National Aeronautics and Space Administration NASA Technical Note
NASA TN D-1921: Handling qualities and trajectory requirements for terminal lunar handling as determinated from analog simulation by Gene J. Matranga 33p NASA TN D-1922: Flight test of a pitch control for a spinning vehicle by H. D. Garner 13p NASA 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 NASA TN D-1924: Rough air effect on crew performance during a simulated low altitude high speed survelliance mission by George J. Hurt 22p NASA Tn D-1925: An analysis of VG and VGH operational data from a twin engine turboprop transport airplane by Paul A. Hunter 45p NASA 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 NASA TN D-1928: Arrest of a moving mass by an attached membrane by Manual Stein 13p NASA 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 NASA 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
Subject Headings:
Thermal;
Copy Details:
Acc. No.: 65582, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA Technical note D 1921-1930
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NASA TN D-1921: Handling qualities and trajectory requirements for terminal lunar handling as determinated from analog simulation by Gene J. Matranga 33p NASA TN D-1922: Flight test of a pitch control for a spinning vehicle by H. D. Garner 13p NASA 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 NASA TN D-1924: Rough air effect on crew performance during a simulated low altitude high speed survelliance mission by George J. Hurt 22p NASA Tn D-1925: An analysis of VG and VGH operational data from a twin engine turboprop transport airplane by Paul A. Hunter 45p NASA 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 NASA TN D-1928: Arrest of a moving mass by an attached membrane by Manual Stein 13p NASA 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 NASA 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
Subject Headings:
Thermal;
Copy Details:
Acc. No.: 65582, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA Technical note D 1921-1930
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