Data reduction system for the Modular Auroral Probe.
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
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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
Modular space station study of environmental control and life support system for long term mission
Modular system-oriented discharge-charge controller for automated space power-source evaluation
Critical mass experiments to establish design calculation standards for modular cavity reactors of gas core nuclear rocket engines
Design, development, and characteristics of modular spaceborne data processors for space shuttle applications
NASA modular aerospace computer for attitude control high speed computation, describing implementation with LSI functional characters
Modular computer design for long term missions, discussing reliability estimation
Earth orbital space stations modular design, discussing space shuttle use, crew training and program management
Space station assembly in earth orbit, providing low transportation costs, modular elements return and incremental growth
Progress in the modular space station development program is reported. The space station project office organization and the manner in which the center interfaces with NR are presented along with a sortie and experiment analysis. The operations, subsystems and configurations are reviewed, and future activities are listed.
The general, operational, design/construction, and subsystem design requirements are presented for a solar powered modular space station system. While these requirements apply only to the initial station system, the system is readily adaptable to a growth configuration.