Minimum-fuel Attitude Control of a Rigid Body in Orbit by an Extended Method of Steepest-descent
Minimum fuel control of spacecraft in orbit using extended method of steepest descent
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Minimum fuel control of spacecraft in orbit using extended method of steepest descent
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Sealing coefficient of visco seal for laminar and turbulent flow, noting Reynolds number effect
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Day and nighttime electron and ion density profiles in lower ionosphere deduced from blunt probe theory and measurements
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Testing technique permits accurate measurement of temperature-dependent thermal conductivity, by virtue of the small temperature differential required across a specimen. The permissible mean insulation temperature ranges from cryogenic to 10 degrees F for the insulation under test.
Ionizable constituent density measurement of D region using Lyman-alpha source and blunt probe