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Gould, L. M.

Publications and source records attributed to Gould, L. M..

Applications technology satellites advanced mission study

Three spacecraft configurations were designed for operation as a high powered synchronous communications satellite. Each spacecraft includes a 1 kw TWT and a 2 kw Klystron power amplifier feeding an antenna with multiple shaped beams. One of the spacecraft is designed to be boosted by a Thor-Delta launch vehicle and raised to synchronous orbit with electric propulsion. The other two are inserted into a elliptical transfer orbit with an Atlas Centaur and injected into final orbit with an apogee kick motor. Advanced technologies employed in the several configurations include tubes with multiple stage collectors radiating directly to space, multiple-contoured beam antennas, high voltage rollout solar cell arrays with integral power conditioning, electric propulsion for orbit raising and on-station attitude control and station-keeping, and liquid metal slip rings.

Gould, L. M.↗

Coded communication link for an advanced manned spacecraft.

An analysis, in terms of key design parameters, is presented of a digital link for bidirectional communication between an advanced manned spacecraft, such as the space shuttle, and a ground terminal by means of a synchronous communication relay satellite. Performance of both ground to manned spacecraft and return links are compared with and without coding. A breadboard terminal for simulating the two-way link is described. Results of error rate tests are discussed.

Gould, L. M.↗