A supercircular entry guidance concept designed for maximum monitoring capability
Reentry vehicle guidance system for automatic or manual range control and with pilot monitoring capability
GUIDANCE SYSTEM↗
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Results for “maximum”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A study of parameters affecting the maximum voltage capabilities of shielded negative dielectric junction vacuum insulators.
Effectiveness parameters of spherical shield electrode surrounding negative dielectric junction of insulator in high vacuum
VACUUM EFFECT↗
Study and analysis of satellite power systems configurations for maximum utilization of power fourth quarterly progress report, 19 feb. - 18 may 1966
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Source record↗
Welded transition joints of 9 Cr-1 Mo alloy steel/316SS for short life /100 hours maximum/ application
Welding parameters and elevated temperature aging and strength characteristics of transition joints between chromium molybdenum alloy steel and stainless steel
WELDING↗
Computerized visibility calculations maximum sighting range program
Computer programs for performance of visibility calculations
COMPUTER PROGRAM↗
Study and analysis of satellite power systems configurations for maximum utilization of power Technical report, 18 May 1965 - 18 Jul. 1966
Optimization of solar cells and radioisotope thermioelectric generators for satellite power supply systems
SOLAR CELL↗
Two-dimensional, hypersonic wings of maximum lift-to-drag ratio.
Slender two-dimensional wing lift-drag ratio at hypersonic speed maximized, assuming modified pressure coefficient
PRESSURE COEFFICIENT↗
Maximum lift-to-drag ratio of a slender, flat-top, hypersonic body.
Lift-drag ratio attainable by slender flat-top body at supersonic speeds, considering Newtonian pressure distribution and constant skin friction
NEWTONIAN FLUID↗
Study and analysis of satellite power systems configurations for maximum utilization of power quarterly progress report, 28 nov. 1966 - 28 may 1967
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Leisenring, J. G.↗
Analytical determination of radial inflow turbine design geometry for maximum efficiency
Optimum design geometry for high radial inflow turbine performance efficiency
Rohlik, H. E.↗
Taking into account the vertical drift of molecular ions when determining the kinetic parameters of ionization-recombination processes in the F2-layer maximum
Height distribution analysis for kinetic molecular ionization-recombination processes in F 2 region during solar activities
Klimov, N. N.↗
Analysis of polar cap absorption events. 3 - Time relation of RF-H alpha maximum intensity for all cm bursts more than or equal to 500 times 10-22 W/m2c/s/-1 Quarterly report
Spectrum analysis of radio frequency emissions from polar cap absorption events
Jonah, F. C.↗
Conical bodies of given length and volume having maximum lift-to-drag ratio at hypersonic speeds - Direct methods
Lift to drag ratios of slender, conical bodies flying at hypersonic speeds, and effects of geometric parameters on aerodynamic stability
Heideman, J. C.↗
Analysis of the maximum performance of a paraboloidal solar collection system for space power
Parametric analysis of effects of concentrator surface errors and rim angle, collection system orientation error, and receiver temperature on paraboloid solar collector thermal efficiency
Kaykaty, G. N.↗
Guidance, flight mechanics and trajectory optimization. Volume 7 - The Pontryagin maximum principle
Maxima-minima theory, Pontryagin principle, and calculus of variations for optimal trajectory and control analysis
Mc Intyre, J. E.↗
The design of a new solid state electronic iterative differential analyzer making maximum use of integrated circuits
Design criteria for solid state electronic, high speed iterative differential analyzer using integrated circuits
Conant, B. K.↗
Variational approach to conical bodies having maximum lift-to-drag ratio at hypersonic speeds
Lift drag ratio attainable by slender conical bodies at hypersonic speeds
Huang, H.-Y.↗
Conical bodies of given length and volume having maximum lift-to-drag ratio at hypersonic speeds. Variational methods
Variational calculus used in obtaining lift drag ratio attainable by slender conical body at hypersonic speeds
Huang, H.-Y.↗