Add to ORKGThe C-band translator, transmitter, and attenuator are described for the spacecraft communication terminal breadboard components. The block diagram is also included for the C-band receiver. The system performance data and the mechanical properties of the system are briefly considered
A prototype coaxial cable bus communication system used in the Trend Monitoring System to interconne...
Aircraft terminal designs for experimental and operational supersonic transport for L band satellite...
A prototpye coaxial cable bus communications system was designed to be used in the Trend Monitoring ...
The design and development of the communications terminal breadboard for the modular space station a...
A baseline design is presented of a digital communications link between an advanced manned spacecraf...
An initial definition of on-board processing requirements for an advanced satellite communications s...
General spacecraft operational characteristics of the Communications Technology Satellite are discus...
The information management systems designed for the modular space station are discussed. Subjects pr...
The design, development, and evaluation of the digital data bus breadboard for the modular space sta...
Summary information on the final communication system design, communication payload, space vehicle, ...
The launch schedule for the Advanced Communication Technology Satellite (ACTS) spacecraft did not le...
Tradeoff analyses on C and X band frequencies for ground-manned spacecraft communications, and trans...
Combined integrated and discrete circuit breadboard model for redundant multiple logic version of Ma...
Electrical components and solid state circuitry decribed for S-band televission transmitte
The results and conclusions of an engineering study of Space Station communications subsystem checko...
A prototype coaxial cable bus communication system used in the Trend Monitoring System to interconne...
Aircraft terminal designs for experimental and operational supersonic transport for L band satellite...
A prototpye coaxial cable bus communications system was designed to be used in the Trend Monitoring ...
The design and development of the communications terminal breadboard for the modular space station a...
A baseline design is presented of a digital communications link between an advanced manned spacecraf...
An initial definition of on-board processing requirements for an advanced satellite communications s...
General spacecraft operational characteristics of the Communications Technology Satellite are discus...
The information management systems designed for the modular space station are discussed. Subjects pr...
The design, development, and evaluation of the digital data bus breadboard for the modular space sta...
Summary information on the final communication system design, communication payload, space vehicle, ...
The launch schedule for the Advanced Communication Technology Satellite (ACTS) spacecraft did not le...
Tradeoff analyses on C and X band frequencies for ground-manned spacecraft communications, and trans...
Combined integrated and discrete circuit breadboard model for redundant multiple logic version of Ma...
Electrical components and solid state circuitry decribed for S-band televission transmitte
The results and conclusions of an engineering study of Space Station communications subsystem checko...
A prototype coaxial cable bus communication system used in the Trend Monitoring System to interconne...
Aircraft terminal designs for experimental and operational supersonic transport for L band satellite...
A prototpye coaxial cable bus communications system was designed to be used in the Trend Monitoring ...