Modular computer research
Onboard modular computer research in strapdown guidance technology for computational ability and long term reliability of unmanned missions
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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.
Contract engineering item specifications for the modular space station are presented. These specifications resulted from the development and allocations of requirements which are concise statements of performance or constraints on performance. Specifications contain requirements for functional performance and for the verification of design solutions.
The orbiting laboratory which can take many forms and can be configured to house a crew of up to 12 men is discussed. The initial study of the 33-foot-diameter Space Station, launched by the Saturn INT-21 and supporting a complement of 12 crewmen, has been completed and documented. A Modular Space Station comprised of smaller, shuttle-launched modules is described. These modules could ultimately be configured to provide for a crew of the same size as envisioned for the 33-foot-diameter Space Station-but buildup would be gradual, beginning with a small initial crew and progressing toward greater capability by adding modules and crewmen on a flexible schedule.
The mission analysis on the modular space station considers experimental requirements and options characterized by low initial cost and incremental manning. Features that affect initial development and early operating costs are identified and their impacts on the program are assessed. Considered are the areas of experiment, mission, operations, information management, and long life and safety analyses.
A modular approach for assessing the affects of radiation environments on man in operational systems has been developed. The feasibility of the model has been proved and the practicality has been assessed. It has been applied to one operational system to date and information obtained has been submitted to systems analysts and mission planners for the assessment of man's vulnerability and impact on systems survivability. In addition, the model has been developed so that the radiobiological data can be input to a sophisticated man-machine interface model to properly relate the radiobiological stress with other mission stresses including the effects of a degraded system.