METEOROID PROTECTION FOR SPACE RADIATORS
Protection of dissipative heat radiators in electric propulsion systems against meteoritic impacts encountered in space travel
METEORITIC DAMAGE↗
SEARCH · Engineering Papers
Results for “Protection”
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
PROTECTION REQUIREMENTS FOR THE RESISTANCE OF METEORITE PENETRATION OF INTERPLANETARY SPACECRAFT SYSTEMS
Protection requirements for the resistance of meteorite penetration damage for various interplanetary spacecraft systems
METEORITIC DAMAGE↗
ARTIFICIAL ELECTRON-BELT RADIATION PROTECTION FOR THE EXPLORER XVI SOLAR CELL POWER SUPPLY
Quartz window thickness requirement to protect explorer xvi solar cells from the artificial radiation belt caused by a high-altitude nuclear explosion
SOLAR CELL↗
INCREASING THE FAR-ULTRAVIOLET REFLECTANCE OF SILICONOXIDE-PROTECTED ALUMINUM MIRRORS BY ULTRAVIOLET IRRADIATION
Visible and uv reflectance and solar absorptance of silicon oxide-protected aluminum mirrors, showing effects of silicon oxide evaporation conditions and ultraviolet irradiation
ULTRAVIOLET RADIATION↗
PROTECTING EXPLORER XVI SOLAR CELLS
Protecting explorer xvi solar cells against increased radiation damage
SOLAR CELL↗
Human vibration and impact protection by airbag restraint systems
Elastic airbag restraint systems for vibration and impact protection of astronauts or aircraft passengers
IMPACT↗
Improved holder protects crystal during high acceleration and impact
A plastic holder, which retains a crystal blank with standard silvered contacts sandwiched between two copper contacts, protects the crystal against vibration during high acceleration and impact.
Le Vay, K. H.↗
Aluminum alloys protected against stress- corrosion cracking
Topcoat of epoxy-polyamide paint is effective protection for aluminum alloys against stress corrosion cracking. The paint can be used on unprimed surfaces.
Source record↗
Wire mesh isolator protects sensitive electronic components
Sensitive electronic components are enclosed in wire mesh for protection. The wire mesh isolates the component from shock and vibration. It acts as a heat sink and as a screen against RF interference.
Kerley, J. J., Jr.↗
Burst diaphragm protects vacuum vessel from internal pressure transients
Supported dual-mode burst diaphragm protects vacuum vessels from transient internal pressures. It forms the interface between the vacuum in the vessel and an external pressure.
Hotz, G. M.↗
Hollow plastic hoops protect thermocouple in storage and handling
Thermocouples are shipped and stored in hollow plastic hoops. The hoop is an inexpensive but efficient method of protection.
Osmond, L. H.↗
Adherent protective coatings plated on magnesium-lithium alloy
Zinc is plated on a magnesium-lithium alloy by using a modification of the standard zinc-plate immersion bath. Further protection is given the alloy by applying a light plating of copper on the zinc plating. Other metals are plated on the copper by using conventional plating baths.
Source record↗
Increasing resistance as a means of providing biological protection against various environmental factors during flight
Increasing resistance for protection against physiological hazards in flight
FLIGHT SAFETY↗
Radiation reactions and chemical protection of animals exposed to high-energy protons
Radiation reactions and chemical protection of animals exposed to high energy protons
HIGH ENERGY↗
Feasibility study of techniques to protect mechanisms operating in space from malfunction. part ii- experimental results and recommendations final report, 8 jun. 1963 - 27 jun. 1964
Various techniques used to protect mechanisms operating in space from malfunctions due to friction
SPACE ENVIRONMENTAL LUBRICATION↗
Performance evaluation of 'thermo-lag' material for entry heat protection of advanced manned spacecraft. vol. 1- summary of investigations final report, 1 oct. 1962 - 31 jan. 1964
Thermoconductivity and thermal properties of protective coating and structural material for reentry manned spacecraft
STRUCTURAL MATERIAL↗
Performance evaluation of ''thermo-lag'' material for entry heat protection of advanced manned spacecraft. vol. 2- thermal investigations final report, 1 oct. 1962 - 31 jan. 1964
Thermal properties and performance of Thermo-lag material for entry heat protection of manned spacecraft
MANNED SPACECRAFT↗
Performance evaluation of ''thermo-lag'' material for entry heat protection of advanced manned spacecraft. vol. 3- structural investigations final report, 1 oct. 1962 - 31 jan. 1964
Mechanical properties and structural analysis of Thermo-lag material for entry heat protection of manned spacecraft
MANNED SPACECRAFT↗