000			02772nam a22003017a 4500
003			OSt
040			_cIIT Kanpur
041			_aeng
110			_a Washington. National Aeronautics and Space Administration (NASA).
245			_aNASA Technical Note [D-3491-3500]
260			_aWashington _bNational Aeronautics and Space Administration (NASA) _c1971
440			_aNational Aeronautics and Space Administration (NASA)
440			_a NASA Technical Note.
500			_aNASA Technical Note [D-3491]: Temperature control unit for sounding rocket applications/ by kerstin Fredga and Robert S. Lee
500			_aNASA Technical Note [D-3492]: Approximation of reentry angles of attack for a spinning body from rate-gyro and accelerometer data/ by Charles H. Whitlock
500			_aNASA Technical Note [D-3493]:Low-speed tests of 50 degree-swept parawings applied to a 0.17-scale model of a manned flight vehicle/ by Frank M. Bugg
500			_aNASA Technical Note [D-3494]: Error detection and correction approach to the time decoding problem/ by A.M. Demmerle, T. J. Karras, and P. J. McCeney
500			_aNASA Technical Note [D-3495]: Analysis of tailored-interface operation of shock tubes with helium-driven planetary gases/ by William J. Loubsky and John O. Reller
500			_aNASA Technical Note [D-3496]: Gemini spacecraft parachute landing system/ by John Vincze
500			_aNASA Technical Note [D-3497]: On the dynamics of capillaries and the existence of plasma flow in the pericapillary lymph space/ by John T. Howe and Yvonne S. Sheaffer
500			_aNASA Technical Note [D-3498]: Flutter at mach 3 of thermally stressed panels and comparison with theory for panels with edge rotational restraint/ by John L. Shideler, Sidney C. Dixon, and Charles P. Shore
500			_aNASA Technical Note [D-3499]: Dynamic-model study of planetary-entry configurations in the langley spin tunnel/ Peter J. Costigan
500			_aNASA Technical Note [D-3500]: Supersonic flutter of flat rectangular orthotropic panels elastically restrained against edge rotation/ by Larry L. Erickson
650			_aTension Shells
653			_aSounding Rocket-- Experiments _aRate-Gyro and Accelerometer Data _aLow-Speed Wind-Tunnel --Investigation _aTime Decoding Problem _aTailored Operation -- Shock Tube _aGemini Landing System _aCapillary Endothelium _aThermal Stress-- Effect _aLangley Spin Tunnel _aSupersonic Flutter
700			_aFredga, kerstin _aLee, Robert S. _aWhitlock, Charles H. _aBugg, Frank M. _aDemmerle, A.M. _aKarras, T. J. _aMcCeney, P. J. _aLoubsky, William J. _aReller, John O. _aVincze, John _aHowe, John T. _aSheaffer, Yvonne S. _aShideler, John L. _aDixon, Sidney C. _aShore, Charles P. _aCostigan, Peter J. _aErickson, Larry L.
942			_cBK
999			_c565871 _d565871