Investigation of the reliability of sterile insertion techniques for spacecraft Final report
Gnotobiotic insertion technique reliability in spacecraft sterilization applications
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Gnotobiotic insertion technique reliability in spacecraft sterilization applications
Thermistor mount for dc potentiometer insertion loss test set
Guidance laws for propellant efficiency with optimum thrust program and error analysis for Voyager mission orbit insertion
Frequency response of forced flow single tube boiler with inserts
Insertion ship tracking errors effect on Apollo Go, No-Go decision making
Reactivity insertions in compact reactor cores due to fuel movement
Failure analysis of Delron inserts in 60B20217-2 heat shield panel
Composite material development and structural design of improved throat inserts for ablative thrust chambers
Neutronic effects of yttrium hydride moderator insertion in fast spectrum reactors
Single tube-in-shell water-boiling heat exchanger performance with helical wire insert and flow stabilizing devices
Real time targeting for Apollo lunar orbit insertion maneuver burn, discussing impulsive maneuvers for flight control
Test device which introduces either pressure or vacuum into a test pipe or tube, is insertable into the tested item where it secures itself into position and requires no external support. The unit has an operating range from zero to 25,000 psig and to any vacuum level that available equipment can reach.
Development of sterile insertion heat sealing tool and port opening
Frequency response of forced flow single tube boiler with inserts and exit restriction
Nozzle insert evaluation and gas cooling concept in storable liquid propellant rocket engine
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