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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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Mercury corrosion and evaluation of corrosion products found in separators of three chromium molybdenum alloy boiling thermal convection loops
Minimal energy ballistic trajectories for manned and unmanned space flights to Mercury
Thermodynamic properties of liquid metal solutions in sodium-mercury system at high temperature
Dynamic pressure relative to inlet vapor flow rate disturbance for mercury vapor condenser
Conceptual and mechanical design analyses, and fabrication of noncondensing radiator for environmental testing of space power mercury Rankine system
Flow meter and prototype mercury propellant feed system
Bibliography and author on Mercury surface, atmosphere, rotation, temperature, and terrain
Radar observations of Mercury have disclosed that the sidereal period of the planet's axial rotation is 59 + 3 days (Pettengill and Dyce, 1965; Dyce et al., 1966), rather than the previously accepted period of 88 days (see, for example, Dollfus, 1953). The purpose of our investigation is to discover the implications for our theories of the solar system (and of the inner planets in particular) which this new result may require.
Local heat transfer and static pressure data for mercury condensing single tube heat exchangers cooled by sodium potassium
Intrinsic photoconductivity and infrared quenching regularity in mercury sulfide crystals with copper and silver impurities within framework of semiconductor model
High speed motion picture study of condensing mercury vapor in glass tubes in ground and zero gravity test facilities
Afterbody heating by Mercury spacecraft during reentry determined from skin temperatures
Cathode durability tests in mercury electron bombardment ion thrustor
Full-scale flight test from sea level of abort- escape system for manned Mercury capsule
Compilation of wind-tunnel heat-transfer measurements on afterbody of Mercury capsule reentry configuration
Afterbody pressure and heat transfer distribution, shock wave shapes, and photographs of local flow conditions for Mercury type capsule at Mach number 15 in helium
Flight test of Little Joe boosted full-scale spacecraft model and escape system for Mercury project
Static aerodynamic characteristics of modified Mercury exit and escape capsule configurations at Mach numbers 3.0 to 6.8