Thermochemical ablation of rocket nozzle insert materials Final report
Resistance of rocket nozzle throat insert materials to corrosion and melting
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Resistance of rocket nozzle throat insert materials to corrosion and melting
Evaluation of bleed insert configuration of single stage axial flow compressor
Rocket nozzle throat insert encapsulated in solid tungsten case
Outer case bleeding or blowing effects on casing insert of single stage axial flow compressor with distorted inlet flow
Throat and nozzle insert design for ablative rocket engine using storable propellants
Radome material insertion loss measurement by radiometric method noting error analysis
Dual channel waveguide insertion loss test set for calibrations at 90 GHz in radio astronomy and communication systems, using sprayed thermistor mount
Real time targeting for Apollo lunar orbit insertion maneuver burn, discussing impulsive maneuvers for flight control
Wire reinforced zirconium oxide rocket nozzle inserts
Neutron and gamma measurements for NASA Plum Brook Reactor HB-6 beam hole insertion facility
Effect of helical flow inserts on boiling pressure drop
Enhanced heat transfer in tubes by using helical vane inserts
Impulsive velocity requirements for insertion into orbits about Venus, Mars, and Jupiter
Water and alkali metal boilers, predicting helical-flow-promoting inserts effect on pressure drop penalties by constant slip model
Tube heat transfer augmentation by helical vane inserts, noting Reynolds number and mass flow rate effects
Technique for sterile insertion of liquids into previously sterilized spacecraft
High impedance alternating current sensing transformer device between two bolometers for measuring insertion loss of test component
Initial data for space shuttle orbiter guidance, navigation, and control equations for preflight, boost, separation, orbit insertion, and ascent abort phases