Nasa technical note [NASA TN D 2861-2870]
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.- Washington, D. C.: National Aeronautics and Space Administration, 1965
.- ( National Aeronautics and Space Administration NASA Technical Note
NASA TN D-2861: Application of Intrinsic differentiation to orbital problems involving curvilinear coordinate systems by James C. Howard 26p NASA TN D-2862: Evaluation of two direct current methods of plasma production for use in magnetic mirror experiments by Roman Krawec 26p NASA TN D-2863: NASA pert time II by Ross C. Bainbridge 19p NASA TN D-2864: Partial experience with the x-15 reaction control and reaction augmentation systems by Calvin R. Jarvis 48p NASA TN D-2865: Exploratory study of bend ductility study of selected refractory metal weldments by John H. Sinclair 27p NASA TN D-2866: Experimental verification of an analytical determiniation of overall thermal conductivity of honeycomb core panels by C. W. Stroud 13p NASA TN D-2867: Convective and eqilibrium radiation heat transfer predictions for project fire reentry vehicle by P. Calvin Stainback 74p NASA TN D-2868: Arc jet thrustor for space propulsion by Lewis E. Wallner 69p NASA TN D-2869: An iterative guidance scheme and its application to lunar landing by Helmut J. Horn 30p 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
Subject Headings:
Orbital problems;
Copy Details:
Acc. No.: 64287, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D 2861-2870
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NASA TN D-2861: Application of Intrinsic differentiation to orbital problems involving curvilinear coordinate systems by James C. Howard 26p NASA TN D-2862: Evaluation of two direct current methods of plasma production for use in magnetic mirror experiments by Roman Krawec 26p NASA TN D-2863: NASA pert time II by Ross C. Bainbridge 19p NASA TN D-2864: Partial experience with the x-15 reaction control and reaction augmentation systems by Calvin R. Jarvis 48p NASA TN D-2865: Exploratory study of bend ductility study of selected refractory metal weldments by John H. Sinclair 27p NASA TN D-2866: Experimental verification of an analytical determiniation of overall thermal conductivity of honeycomb core panels by C. W. Stroud 13p NASA TN D-2867: Convective and eqilibrium radiation heat transfer predictions for project fire reentry vehicle by P. Calvin Stainback 74p NASA TN D-2868: Arc jet thrustor for space propulsion by Lewis E. Wallner 69p NASA TN D-2869: An iterative guidance scheme and its application to lunar landing by Helmut J. Horn 30p 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
Subject Headings:
Orbital problems;
Copy Details:
Acc. No.: 64287, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D 2861-2870
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