000 | 02057nam a22002897a 4500 | ||
---|---|---|---|
003 | OSt | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
245 | _aNASA Technical Note [D- 251-260] | ||
260 |
_aWashington _bNASA _c1960 |
||
440 | _aNational Aeronautics and Space Administration | ||
440 | _aNASA Technical Note | ||
500 | _aNASA TN D-251 -- A summary of operating conditions experienced by two helicopters in a commercial and a military operation/ Andrew B. Connor and LeRoy H. Ludi | ||
500 | _aNASA TN D-252 -- Investigation of the natural frequencies of fluids in spherical and cylindrical tanks/ John Locke McCarty and David G. Stephens | ||
500 | _aNASA TN D-253 -- Longitudinal range control during the atmospheric phase of a manned satellite reentry/ Arthur Assadourian and Donald C. Cheatham | ||
500 | _aNASA TN D-254 -- An analysis of nose ablation for ballistic vehicles/ Leonard Roberts | ||
500 | _aNASA TN D-255 -- Requirements of trajectory corrective impulses during the approach phase of an interplanetary mission/ Alan L. Friedlander and David P. Harry, III | ||
500 | _aNASA TN D-256 -- Fatigue damage during complex stress histories/ H. W. Liu and H. T. Corten | ||
500 | _aNASA TN D-257 -- Performance investigation of a nonpumping rocket-ejector system for altitude simulation/ Anthony Fortini | ||
500 | _aNASA TN D-258 -- Propellant vaporization as a criterion for rocket-engine design: experimental effect of combustor length, throat diameter, injection velocity, and pressure on rocket combustor efficiency/ Bruce J. Clark | ||
500 | _aNASA TN D-259 -- Rolling-contact fatigue life of a crystallized glass ceramic/ Thomas L. Carter and Erwin V. Zaretsky | ||
500 | _aNASA TN D-260 -- Continued study of advanced-temperature nickel-base alloys to investigate vanadium additives/ John C. Freche, Thomas J. Riley and William J. Waters | ||
650 | _aAeronautics | ||
650 | _aSpacecraft | ||
942 | _cBK | ||
999 |
_c565851 _d565851 |