000 -LEADER |
fixed length control field |
01933nam a22003017a 4500 |
003 - CONTROL NUMBER IDENTIFIER |
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OSt |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20220713112636.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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220713b 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 2861-2870] |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
Place of publication |
Washington, D. C. |
Name of publisher |
National Aeronautics and Space Administration |
Year of publication |
1965 |
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-2861: Application of Intrinsic differentiation to orbital problems involving curvilinear coordinate systems by James C. Howard 26p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2862: Evaluation of two direct current methods of plasma production for use in magnetic mirror experiments by Roman Krawec 26p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2863: NASA pert time II by Ross C. Bainbridge 19p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2864: Partial experience with the x-15 reaction control and reaction augmentation systems by Calvin R. Jarvis 48p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2865: Exploratory study of bend ductility study of selected refractory metal weldments by John H. Sinclair 27p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2866: Experimental verification of an analytical determiniation of overall thermal conductivity of honeycomb core panels by C. W. Stroud 13p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2867: Convective and eqilibrium radiation heat transfer predictions for project fire reentry vehicle by P. Calvin Stainback 74p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2868: Arc jet thrustor for space propulsion by Lewis E. Wallner 69p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2869: An iterative guidance scheme and its application to lunar landing by Helmut J. Horn 30p |
500 ## - GENERAL NOTE |
General note |
NASA TN D-2870: Effect of high velocity fluid flow on the bending vibrations and ststic divergence of a simply supportd pipe by Harold L. Dodds 10p |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical Term |
Orbital problems |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Technical Report |