Design, development, and fabrication of a functional adhesive bonding repair experiment to be performed during space flight Final report, Nov. 1966 - May 1968
Adhesive repair system for application in weightless vacuum space environment
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Adhesive repair system for application in weightless vacuum space environment
Network logic design for data commutation functions in self repairable computer multiprocessor
Porosity, mismatch and repair of aluminum weldments
Hand-operated tool repairs weld defects in large-diameter, thin-walled stainless steel tubes. Tool consists of a three-roll external planisher and an internal backup mandrel, both hydraulically pressurized by hand pumps, and an external restraining mandrel, which keeps the tube from turning during the planishing operations.
Two versions of a portable tool repair the seats of tube fittings and the flared ends of tubing. Each version operates on the principle of lapping to remove imperfections from tube and fitting interfacing surfaces.
Mechanism of DNA repair of radiation injury and survival properties of cells under conditions of normal growth, starvation, and DNP treated
Apollo 11 IRIG repair program emphasizing bearing improvement and contamination control programs
Vacuum jacketed components on launch umbilical tower service arms at Launch Complex 39 - repair techniques for carbon dioxide and vacuum jacketed transfer lines
Resupply and repair capabilities for orbital space station bipropellant propulsion system
Properties, evaluation, inspection, and repair of alloys and silicide coatings for space shuttles
Precision machining and repair of radioactive Plum Brook Reactor core fuel grid
Self testing and repairing computer comprising control and diagnostic unit and rollback points for error correction
Study of short-time high-temperature diffusion treatments as part of a program of development of methods of reapplying fused slurry silicide coating in the field. The metallographic structure and oxidation behavior of R512E applied to Cb-752 coated under simulated field repair conditions was determined. Oxidation testing in reduced pressure environment has shown that performance equivalent to furnace-processed specimens can be obtained in a two-minute diffusion at 2700 F.
Collection of theoretical and experimental studies covering basic mechanisms of fatigue in the subcreep and creep ranges, fatigue damage detection, field practices for fatigue damage repair in jet engine components, and fatigue damage avoidance and control. Individual items are abstracted in this issue.
The MULTIPAC is a central data system developed for deep-space probes with the distinctive feature that it may be repaired during flight via command and telemetry links by reprogramming around the failed unit. The computer organization uses pools of identical modules which the program organizes into one or more computers called processors. The interaction of these modules is dynamically controlled by the program rather than hardware. In the event of a failure, new programs are entered which reorganize the central data system with a somewhat reduced total processing capability aboard the spacecraft. Emphasis is placed on the evolution of the system architecture and the final overall system design rather than the specific logic design.
Sound level measurements on noise sources on buses are used to observe the effects of attenuating acoustic pressure levels inside the bus by sound-proofing during complete repair. A spectral analysis of the sound level as a function of motor speed, bus speed along the road, and the category of the road is reported.
High-temperature, reusable surface insulation tiles are repaired quickly and economically using prefabricated tile plugs.