Add to ORKGThe field of view required of the space base antenna is defined for both the tracking and data relay satellite link and detached module links. The gain requirements are established and the feasibility of alternative antenna configurations using phased arrays and reflectors are considered. One recommended and one alternative configuration are presented for each of the required links
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...
Checkout and data management system requirements for space station and space base mission progra
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...
The configuration and functions of the ITOS D and E system are described. The system will expand the...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
A pre-entry communications study is presented for a relay link between a Jupiter entry probe and a s...
Antenna systems capable of operating with a multichannel microwave radiometer intended for mapping s...
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
Flight dynamics, experiment operational phase sequence, and support operations for Applications Tech...
Application Technology Satellite /ATS/ SPACECRAFT tradeoff and analysis - configuration paraboloid a...
Investigation of cost effective utilization of space maintenance and repair techniques to despin App...
A recommendation for the location of the Space Shuttle C-Band Beacon Antenna(s) to be used during Ap...
Study of design for experimental L band supersonic transport communications/surveillance termina
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...
Checkout and data management system requirements for space station and space base mission progra
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...
The configuration and functions of the ITOS D and E system are described. The system will expand the...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
A pre-entry communications study is presented for a relay link between a Jupiter entry probe and a s...
Antenna systems capable of operating with a multichannel microwave radiometer intended for mapping s...
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
Flight dynamics, experiment operational phase sequence, and support operations for Applications Tech...
Application Technology Satellite /ATS/ SPACECRAFT tradeoff and analysis - configuration paraboloid a...
Investigation of cost effective utilization of space maintenance and repair techniques to despin App...
A recommendation for the location of the Space Shuttle C-Band Beacon Antenna(s) to be used during Ap...
Study of design for experimental L band supersonic transport communications/surveillance termina
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...