Protective coating for refractory metals in rocket engines supplemental report, mar. 8, 1963 - mar. 15, 1964
Protective coating systems for refractory metal used in rocket engine nozzles - rocket engine test firing
TEST FIRING↗
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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.
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Effect of protective coatings on the stress- corrosion properties of supersonic-transport skin materials tenth quarterly status report, 1 mar. - 31 may 1965
Protective coating effect on stress corrosion properties of supersonic transport skin materials - bending-ductility evaluation
PROTECTIVE COATING↗
One-dimensional numerical analysis of the transient response of thermal protection systems
One-dimensional numerical analysis of transient response of thermal protection system
TRANSIENT RESPONSE↗
Effect of protective coatings on the stress- corrosion properties of supersonic-transport skin materials eleventh quarterly status report, 1 jun. - 31 aug. 1965
Protective coatings effect on stress corrosion properties of supersonic transport skin materials
SKIN↗
Apollo space nuclear radiation protection status report
Apollo spacecraft nuclear radiation protection
RADIATION PROTECTION↗
A space radiation protection system for near- earth manned orbital space stations
Space radiation protection system for near earth manned orbital space stations
EARTH ORBIT↗
The effect of meteoroid flux velocity distribution and angle of impact upon the design of spacecraft meteoroid protection systems
Effect of meteoroid flux velocity distribution and angle of impact on design of spacecraft meteoroid protection systems
VELOCITY DISTRIBUTION↗
Meteoroid protection for spacecraft structures final report
Procedure for determination of meteoroid protection requirements for spacecraft structures
SPACECRAFT STRUCTURE↗
Thermal balance and heat protection.
Protection of spacecraft against thermal environment during launching, flight and reentry phases, emphasizing charring and melting ablator systems
THERMAL PROTECTION↗
Performance evaluation of ''Thermo-lag'' material for entry heat protection of advanced manned spacecraft Quarterly progress report, 1 Jan. - 1 Apr. 1963
Environmental, solid-state thermal, and mechanical properties of Thermo-Lag material for entry thermal protection of advanced manned spacecraft
SOLID STATE↗
Performance evaluation of ''Thermo-lag'' material for entry heat protection of advanced manned spacecraft Material development report, 1 Oct. 1962 - 1 Apr. 1963
Performance evaluation of Thermo-lag material for advanced manned spacecraft reentry heat protection
HIGH TEMPERATURE MATERIAL↗
High temperature protective coatings for refractory metals Progress report no. 3, 1 May - 31 Jul. 1965
High temperature protective coating for refractory metals - electrodeposition and diffusion bonding of iridium on tantalum to prevent oxidation
TANTALUM↗
An analysis of a charring ablation thermal protection system
Analytical model for predicting transient one- dimensional thermal performance of charring- ablator heat-protection system exposed to hyperthermal environment
THERMAL PROTECTION↗
Self-sealing shields for micrometeorite protection
Self-sealing shields for micrometeorite protection of spacecraft cryogenic propellant tanks
SHIELDING↗
Injurious effect of 660 and 120 MeV protons and the efficacy of pharmacological and chemical protection
Pharmacological and chemical protection for mice exposed to 120 and 660 MeV protons
MOUSE↗
New ways of studying chemical protection against genetic changes
Radiation protection offered by pyrimidine base analogs and aminothiol compounds against genetic changes in Escherichia coli exposed to X-ray irradiation
RADIATION PROTECTION↗
High temperature protective coatings for refractory metals Yearly summary report, 21 Oct. 1964 - 21 Oct. 1965
Performance characteristics of iridium used as high temperature oxidation protective coating for refractory metals
PROTECTIVE COATING↗
Effects of Commercially Available Protective Coatings on Stress-corrosion Properties of Supersonic-transport Skin Materials Final Summary Report, 1 Jun. 1964 - 31 Jan. 1966
Protective coating effect on stress corrosion properties of supersonic transport skin materials
PROTECTIVE COATING↗