000			01933nam a22003017a 4500
003			OSt
005			20220713112636.0
008			220713b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administration
245			_aNasa technical note [NASA TN D 2861-2870]
260			_aWashington, D. C. _bNational Aeronautics and Space Administration _c1965
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical Note
500			_aNASA TN D-2861: Application of Intrinsic differentiation to orbital problems involving curvilinear coordinate systems by James C. Howard 26p
500			_aNASA TN D-2862: Evaluation of two direct current methods of plasma production for use in magnetic mirror experiments by Roman Krawec 26p
500			_aNASA TN D-2863: NASA pert time II by Ross C. Bainbridge 19p
500			_aNASA TN D-2864: Partial experience with the x-15 reaction control and reaction augmentation systems by Calvin R. Jarvis 48p
500			_aNASA TN D-2865: Exploratory study of bend ductility study of selected refractory metal weldments by John H. Sinclair 27p
500			_aNASA TN D-2866: Experimental verification of an analytical determiniation of overall thermal conductivity of honeycomb core panels by C. W. Stroud 13p
500			_aNASA TN D-2867: Convective and eqilibrium radiation heat transfer predictions for project fire reentry vehicle by P. Calvin Stainback 74p
500			_aNASA TN D-2868: Arc jet thrustor for space propulsion by Lewis E. Wallner 69p
500			_aNASA TN D-2869: An iterative guidance scheme and its application to lunar landing by Helmut J. Horn 30p
500			_aNASA 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			_aOrbital problems
942			_cTR
999			_c565875 _d565875