000			01762nam a22002897a 4500
003			OSt
005			20230118160918.0
008			230118b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administration
245			_a-
260			_aWashington, D. C. _bNational Aeronautics and Space Administration _c1969
300			_a33p
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical Note
500			_aNASA TN D-4891: Prediction of lift and drag for slender sharp-edge delta wings in ground proximity by Charles H. Fox 33p
500			_aNASA TN D-4892: Rotational and vibrational temperature measurements in the 12-inch hypersonic ceramic heated tunnel by John C. Hope 35p
500			_aNASA TN D-4893: Analysis of commutated networks employing feedback circuits by Michael T. Borelli 85p
500			_aNASA TN D-8994: Blast shields testing by Walter V. Medenica 59p
500			_aNASA TN D-4895: Optimum design of communication links with noisy phase reference by William E. Zurubek 22p
500			_aNASA TN D-4896: Response develope- A global description of three axix large angle spacecraft attitutude control systems by George Meyer 31p
500			_aNASA TN D-4897: Transient solidification outside a cooled pipe application to a solar brayton heat receiver by Wellington W. Hu 30p
500			_aNASA TN D-4898: Design and analysis of a modular servoamplifier for fast response electrhydrraulic control systems by John R. Zeller 20p
500			_aNASA TN D-4899: Prediction of thermodynamic effects of developed gavitation based on liquid hydrogen and freon-114 data in scaled ventures by Royce D. Moore 22p
942			_cTR
999			_c566440 _d566440