| 000 -LEADER |
|---|
| fixed length control field |
02100nam a22002897a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
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| control field |
20220715120655.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
220715b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE |
|---|
| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
|---|
| Language code of text/sound track or separate title |
eng |
| 110 ## - MAIN ENTRY--CORPORATE NAME |
|---|
| Corporate name or jurisdiction name as entry element |
Washington: National Aeronautics and Space Administration |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
Nasa technical note [NASA TN D 1921-1930] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington, D.C. |
| Name of publisher |
National Aeronautics and Space Administration |
| Year of publication |
1963 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administration |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Note |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-1921: Handling qualities and trajectory requirements for terminal lunar handling as determinated from analog simulation by Gene J. Matranga 33p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-1922: Flight test of a pitch control for a spinning vehicle by H. D. Garner 13p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-1924: Rough air effect on crew performance during a simulated low altitude high speed survelliance mission by George J. Hurt 22p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA Tn D-1925: An analysis of VG and VGH operational data from a twin engine turboprop transport airplane by Paul A. Hunter 45p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-1928: Arrest of a moving mass by an attached membrane by Manual Stein 13p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Thermal |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
