000 | 02007nam a22002897a 4500 | ||
---|---|---|---|
003 | OSt | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
245 | _aNASA Technical Note [D- 3401-10] | ||
260 |
_aWashington _bNASA _c1966 |
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440 | _aNational Aeronautics and Space Administration | ||
440 | _aNASA Technical Note | ||
500 | _aNASA TN D-3401 -- Aerodynamic characteristics of raked-off circular and elliptical cones at a mach number of 20 in helium/ John K. Molloy | ||
500 | _aNASA TN D-3402 -- Manual abort guidance from the midcourse region of a lunar mission/ George P. Callas and Robert B. Merrick | ||
500 | _aNASA TN D-3403 -- Effect of target angular oscillations on pilot-controlled Gemini-Agena docking/ Donald R. Riley, Byron M. Jaquet and Jere B. Cobb | ||
500 | _aNASA TN D-3404 -- A method of trajectory optimization by fast-time repetitive computations/ Rodney C. Wingrove, James S. Raby and D. Francis Crane | ||
500 | _aNASA TN D-3405 -- Information transfer systems in space communications/ Amadeo Dabul | ||
500 | _aNASA TN D-3406 -- Evaluation of tangential velocity effects on spinning transverse combustion instability/ Marcus F. Heidmann and Charles E. Feiler | ||
500 | _aNASA TN D-3407 -- Thrust measurement of sert I ion thrustors/ William C. Nieberding and Robert R. Lovell | ||
500 | _aNASA TN D-3408 -- Supersonic investigation of effects of configuration geometry on pressure-coefficient and section normal-force-coefficient distributions for a two-stage launch vehicle/ James A. Blackwell | ||
500 | _aNASA TN D-3409 -- Mechanical and physical properties of the echo II metal-polymer laminate/ C. L. Staugaitis and L. Kobren | ||
500 | _aNASA TN D-3410 -- One-dimensional nonlinear model for determining combustion instability in solid propellant rocket motors/ Louis A. Povinelli | ||
650 | _aAeronautics | ||
650 | _aSpacecraft | ||
942 | _cBK | ||
999 |
_c565905 _d565905 |