Extreme temperature requirements for spacecraft electronics parts. FY 69 report - The low temperature case
Extreme temperature determinations which affect spacecraft electronic equipment on flyby missions
Hutchinson, T.↗
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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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A versatile, low cost, fabrication technique for flight hardware
Wiring technique for spacecraft electronic equipment using integrated circuits
Chernikoff, H.↗
Reactor power system/spacecraft integration
The new national initiative in space reactor technology evaluation and development is strongly tied to mission applications and to spacecraft and space transportation system (STS) compatibility. This paper discusses the power system integration interfaces with potential using spacecraft and the STS, and the impact of these requirements on the design. The integration areas of interest are mechanical, thermal, electrical, attitude control, and mission environments. The mission environments include space vacuum, solar input, heat sink, space radiation, weapons effects, and reactor power system radiation environments. The natural, reactor, and weapons effects radiation must be evaluated and combined to define the design requirements for spacecraft electronic equipment.
Elms, R. V.↗
Components irradiation test no. 8 2n918 transistors in250 diodes tantalum capacitors
Radiation effect on electronic equipment for nuclear spacecraft - transistors, diodes, and tantalum capacitors
SPACECRAFT ELECTRONIC EQUIPMENT↗
Pegasus detector system evaluation tool Final report
Test tool to simulate critical portions of Pegasus meteoroid detector electronics
TEST EQUIPMENT↗
The study of multipactor breakdown in space electronic systems Final report
Conditions and causes of multipactor breakdown and discharge in spacecraft electronic systems and equipment
SECONDARY EMISSION↗
COMPUTER DESIGN PROBLEMS FOR THE SPACE ENVIRONMENT
Functional and environmental requirements for spacecraft computer systems in manned and unmanned missions
COMPUTER DESIGN↗
Design of an onboard checkout system.
Onboard checkout equipment design requirements, considering hardware and software for manned spacecraft flight
CHECKOUT EQUIPMENT↗
Marshall Space Flight Center microelectronics program
Marshall Space Flight Center microelectronics program implementation, hardware development, and research and development
MICROMINIATURIZED ELECTRONIC EQUIPMENT↗
Thin-film microcircuit development at Marshall Space Flight Center
Marshall Space Flight Center thin film microcircuit development program
MICROCIRCUIT↗
Research for space enters the electronics age.
Electronic equipment performance and reliability improvement to meet technological advances for deep space communication
SPACE COMMUNICATION↗
Mariner Mars 1964 basic structure, design and development
Structure, design, and fabrication of Mariner IV 1964 spacecraft and electronic assembly
ELECTRONIC EQUIPMENT↗
Acceptance checkout equipment for spacecraft - ACE-S/C.
Acceptance checkout equipment spacecraft for centralized control and LEM and CSM systems testing
SPACECRAFT ELECTRONIC EQUIPMENT↗
The lunar orbiter telecommunications system.
Spacecraft and ground equipment design of lunar orbiter telecommunications system
SPACECRAFT ELECTRONIC EQUIPMENT↗
PILOT MANUFACTURING FOR SPACECRAFT
Spacecraft materials - manufacture of bearings, accelerometers and electronic equipment
MANUFACTURING↗
Fire extinguishment and inhibition in spacecraft environments
It was concluded that it is essential that NASA develop a comprehensive approach to fire extinguishment and inerting in spacecraft environments. Electronic equipment might be easily protected through use of an onboard inert gas generating system. The use of Halon 1301 presents serious technological challenges for agent cleanup and removal of the toxic and corrosive products of combustion. Nitrogen pressurization, while effective, probably presents a serious weight penality. The use of liquid water sprays appears to be the most effective approach to general purpose spacecraft fire protection.
Deris, John↗
ELECTRICAL SYSTEMS IN MISSILES AND SPACE VEHICLES
Missile and space vehicle electrical systems - space science
SPACE VEHICLE CONTROL↗
MICROWAVE RADIOMETER INSTRUMENTATION FOR VENUS STUDIES
Description of a microwave radiometer used on the mariner venus probe
SPACECRAFT ELECTRONIC EQUIPMENT↗