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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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Basic design considerations for a small scientific satellite
Scientific satellite design considerations for spacecraft itself, spacecraft/launch vehicle interface, and ground support equipment and transportation
Fast low-power-drain logic system for use in nuclear experiments on scientific satellites
Scientific satellites nuclear experiments fast low power drain logic system, using AND and NAND gates, pulse generators, delays and bistables
Design considerations for the small scientific satellite
Small scientific satellite design guidelines and concepts, noting flexibility regarding accommodation of variety of missions for magnetosphere studies
The Small Scientific Satellite
Small Scientific Satellite program, discussing payload for investigating magnetosphere and near interplanetary space
THE PURPOSES OF ENVIRONMENT TESTING FOR SCIENTIFIC SATELLITES
Environmental testing for scientific satellite reliability
The purpose of environmental testing for scientific satellites
Environmental test program for scientific satellite reliability evaluation
Telemetry processing for NASA scientific satellites
Telemetry processing for NASA scientific satellites
Telemetry and data processing systems for scientific satellites
Telemetry and data processing systems for scientific satellites
Biomedical Experiments Scientific Satellite /BESS/
The Biomedical Experiments Scientific Satellite (BESS) program is proposed to provide a long-duration, earth-orbiting facility to expose selected specimens in a series of biomedical experiments through the 1980's. Launched and retrieved by the Space Transportation System, the fully reusable, free-flying BESS will contain all systems necessary to conduct a six-month to one-year spaceflight mission. The spacecraft system will consist of a large pressurized experiment module and a standard NASA service module currently conceived as the Goddard Multi-Mission Spacecraft (MMS). The experiment module will contain the life-support systems, waste management system, specimen-holding facilities, and monitoring, evaluating, and data-handling equipment. Although a variety of specimens will be flown in basic biological and medical studies, the primate was taken as the principal design driver since it has a maximal life-support demand.
Quality control and nondestructive testing for the prevention of failures in scientific satellites.
Quality control and nondestructive testing of scientific satellite components stressing adequate standards and contractor responsibility
A new design approach for wide-range temperature monitoring and compensating networks in scientific satellites
Mathematical design model for compensated thermistor networks in scientific satellites
SCIENTIFIC SATELLITES - A PERSPECTIVE KEYNOTE ADDRESS
Engineering problems in scientific satellites electronic apparatus for attitude control & power supply
Introduction to the international scientific satellite ESRO 2/IRIS
Introduction to international scientific satellite ESRO 2/IRIS
Sliding electrical contacts for unmanned scientific satellites
Sliding electrical contacts for unmanned scientific satellites, discussing Nimbus AVCS camera iris motors
High-voltage breakdown problems in Goddard scientific satellites
High voltage breakdown problems in Goddard scientific satellites
Processing of data transmitted by NASA scientific satellites
Processing of data transmitted by NASA scientific satellites