The work performed entailed the design, development, construction and testing of a 4000 word by 18 bit random access, NDRO plated wire memory for use in conjunction with a spacecraft imput/output unit and central processing unit. The primary design parameters, in order of importance, were high reliability, low power, volume and weight. A single memory unit, referred to as a qualification model, was delivered
Airborne/spaceborn computer design and techniques for space shuttle data management system
A software package developed for detection and analysis of infrasounds produced by air turbulence is...
Mod I engine testing and test results, the test of a Mod I engine in the United States, Mod I engine...
In order to prepare a site for a manned lunar base, an autonomously operated construction vehicle is...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
MULTIPAC, multiple pool processor and computer for deep space probe central data syste
D-200 computer family, system error analysis, reliability derivation, and power converter design for...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Circuitry, logical design, and test data on redundant spacecraft sequencer breadboar
The requirements for performance, design, test, and qualification of a computer program identified a...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
Developing structure, payload, communication and data handling subsystems for ERT
The design, development, and implementation of a prototype, partially populated, million bit read-wr...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Voyager spacecraft sterilization - launch area operations, biological barrier, microbiological analy...
Airborne/spaceborn computer design and techniques for space shuttle data management system
A software package developed for detection and analysis of infrasounds produced by air turbulence is...
Mod I engine testing and test results, the test of a Mod I engine in the United States, Mod I engine...
In order to prepare a site for a manned lunar base, an autonomously operated construction vehicle is...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
MULTIPAC, multiple pool processor and computer for deep space probe central data syste
D-200 computer family, system error analysis, reliability derivation, and power converter design for...
Multicomputer configurations and redundancy management techniques used in various airborne systems w...
Circuitry, logical design, and test data on redundant spacecraft sequencer breadboar
The requirements for performance, design, test, and qualification of a computer program identified a...
Activity conducted in the following areas is highlighted: space sciences, space transportation syste...
Developing structure, payload, communication and data handling subsystems for ERT
The design, development, and implementation of a prototype, partially populated, million bit read-wr...
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Voyager spacecraft sterilization - launch area operations, biological barrier, microbiological analy...
Airborne/spaceborn computer design and techniques for space shuttle data management system
A software package developed for detection and analysis of infrasounds produced by air turbulence is...
Mod I engine testing and test results, the test of a Mod I engine in the United States, Mod I engine...