000			01943nam a22003017a 4500
003			OSt
005			20220726130132.0
008			220726b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National aeronautics and Space Administration
245			_aNASA technical note [NASA TN D 2681-2690]
260			_aWashington, D. C. _bNational aeronautics and Space Administration _c1965
440			_aNational aeronautics and Space Administration
440			_aNASA Technical Note
500			_aNASA TN D-2681: Some visual observations of cavitation in rotating machinery by Richard F. Soltis 17p
500			_aNASA TN D-2682: The rocket interferometer tracking (RIT) system by Michael Spafford 24p
500			_aNASA TN D-2863: A method for arraying yagi disk antennas by Fred B. Beck 18p
500			_aNASA TN D-2684: Linear accelation guidance scheme for landing and launch trajectories in a vacuum 18p
500			_aNASA TN D-2685: Sealed foam constrictive wrapped external insulation system for liquid hydrogen tanks of boost vehicles by Lewis Research Center 157p
500			_aNASA TN D-2686: Influence of entrained gases and a halogen additive on boundary lubrication ogf four oils at temperatures to 1000 degree F by Donald H. Buckely 15p
500			_aNASA TN D-2687: Turbulent skin friction at high reynolds numbers and low supersonic velocities by Mary W. Jackson 31p
500			_aNASA TN D-2688: Improved ceramic bonded calcium fluoride coatings for lubricating nickel base alloys in air at temperatures from 500 degree to 1700 degree F
500			_aNASA TN D-2689: Detection of flow field instability in the presence of buffeting by the partial mode model technique by Henry A. Cole 33p
500			_aNASA TN D-2690: Landing gear loads obtained during simulated landing tests over various obstacles by Robert C. Dreber 121p
650			_aObstacles
942			_cTR
999			_c565938 _d565938