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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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Expandable and modular structures for support on manned space missions, reviewing inflatable, chemically rigidizable, unfurlable and elastic recovery structures
Modular 100 MHz digital time analyzer using flexible plug-in logic
Aluminum and magnesium composite sheet laminates reinforced with low density, high strength modular filament sheets are produced by diffusion bonding and explosive bonding. Both processes are accomplished in normal atmosphere and require no special tooling or cleaning other than wire brushing the metal surfaces just prior to laminating.
Three-dimensional modular console prototypes for configuring control and display devices
Large area modular glancing-reflection X ray gathering system for focusing photons in 0.1 to 20,000 ev range, noting improved SNR
Expandable and modular structures for support on manned space missions, reviewing inflatable, chemically rigidizable, unfurlable and elastic recovery structures
Design and analysis of modular servoamplifier for fast response electrohydraulic control systems
Modular three dimensional mockup technique for economizing and facilitating design of control and display equipment
Modular configuration of recoverable scientific MAP /Modular Auroral Probe/ payloads aboard Nike-Apache rockets, discussing payload design concepts
IBM 360-50 computer with I/O terminals to process PCM and analog data from Modular Auroral Probe series of sounding rockets on real time basis
Modularized static AC and DC inverters and converters for aerospace electrical power conditioning systems, discussing circuit functions and performance tests
Data and specifications on thermal protection systems for modular nuclear vehicle
Threshold logic implementation for LSI design of modular computer system
Onboard modular computer research in strapdown guidance technology for computational ability and long term reliability of unmanned missions
Each modular element consists of two hemispherical shells with material removed near their apexes to permit joining by a weldment to form a passage. Elements are welded together at their largest dimensions to form either a straight line continuous or a circular pressure vessel.
Swirl-can modular turbojet combustor burning natural gas fuel
Performance of short modular turbojet combustor segment with ASTM-A1 fuel