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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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Design and fabrication of sterilization container and model probe assembly for Mars landing capsule
Parachute configuration, dummy and modified recorder capsules, and drop tests for parachute recovery system
Electromagnetic blood flow meter to determine blood flow through intact vessels of test animals in gravitational stress and in extraterrestrial space capsules
Absolute electron densities of upper ionospheric F layer by measuring radio phase dispersion between separating rocket capsules
Capsule sterilization, basic concepts, techniques and engineering problems
Modified gloved enclosure is used to fill a capsule with a mixture of americium and beryllium radioactive powders to seal weld the opening, and to test it for leaks. It contains a horizontal partition, vortex mixer, mounting press, welder, test vessel, and radiation shielding to prevent surface contamination.
Sample capsule for determination of oxygen in hemolyzed blood consists of a measured section of polytetrafluoroethylene tubing equipped at each end with a connector and a stopcock valve. This method eliminates errors from air entrainment or from the use of mercury or syringe lubricant.
Various approaches to problems of delivering Apollo type entry capsule to Mars, entering and descending through its atmosphere, and placing scientific payload on its surface
Sterilization plan for Voyager capsule
Power systems related to Mars landing capsule
Instruments for measuring altitude dependent physical properties of Venus atmosphere from entry capsule
Molybdenum alloy /TZM/ capsule experiments with boiling-refluxing potassium to determine mass transfer parameters
Method and computer program for calculating creep and optimizing dimensions of capsules filled with alpha-emitting radioisotopes and exposed to varying stress and temperature
Static aerodynamic characteristics of experimental nonlifting reentry capsule in combination with rocket booster at Mach numbers from 0.60 to 1.20
Full-scale wind tunnel determination of effect of corrugated canister surface on static aerodynamic characteristics of reentry capsule
Feasibility estimate, mission profile, and design Orbital Experiment Capsule /OEC/ Mars satellite to be used in Voyager Project
Venus/Mercury swingby with Venus capsule - preliminary science objectives and experiments for use in advanced mission studies
Aerodynamic, thermodynamic and structural design aspects of flight capsule entering low density Mars atmosphere from orbit