Communications and data handling

Abstract

The communications system for the planetary entry missions is discussed with emphasis on the basic problems of the data link: uncertainty about atmospheric composition, time limitation for transmission, and geometry variation or change in aspect angles. The baseline design for Pioneer is reviewed. In this design, telemetry is transmitted only during the descent phase of probe entry at 44 bits-per-second. It is indicated that this design encompasses different atmospheric entries for different planets, different atmospheric models of planetary atmospheres, and allows for dispersion in the entry angle and phasing. The radio frequency environment is considered to be the prime problem of the communication link, therefore a discussion of the ionospheric absorption and turbulence models is included.