Projected NASA/JPL deep space network capabilities in the 1970's.
Deep space network /DSN/ for navigational and communications support to NASA lunar and planetary space programs
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Deep space network /DSN/ for navigational and communications support to NASA lunar and planetary space programs
At present, there are several models involving the surface, atmosphere (and ionosphere), and cloud conditions of the planet Venus which attempt to account for the observed high brightness temperature of 600 degrees Kelvin in the microwave temperature region. None of these models can be definitely accepted or rejected on the basis of presently available data, and it is the goal of the microwave radiometer experiment planned for the Mariner Venus mission to determine which of the proposed models most nearly approximates Venusian conditions. The disc of the planet will be scanned at 4 wavelengths - 4, 8, 13.5 and 19 millimeters - to measure the temperature distribution across the planet. Measurement accuracy is expected to be to within 2 percent. In addition to the study of gross thermal characteristics of surface and atmosphere (or ionosphere), some information regarding the fine-scale thermal variations will be obtained. Since Venus appears to be continuously covered by clouds, it is obvious that only in the microwave region can one be sure of penetrating clear to the solid surface. Because of the absorbing characteristics of the Earth's atmosphere, and because of the relatively poor resolution obtainable in this region of the spectrum, one is forced to utilize the platform afforded by a planetary flyby or orbiter in order to conduct a reliable high resolution study of the planet. To do so from Earth (neglecting terrestrial atmospheric attenuation ) would require colossal radio telescopes.
Constants and related data used in trajectory calculations at jet propulsion laboratory
Spacecraft look-angle problem - instrument orientation
Mariner /venus 62/ flight telecommunication system for data transmission and trajectory determination
Test equipment, facilities and types of tests involved in system checkout of the ranger and mariner spacecrafts
Mission plans for mariner mars 1964
Telemetry and command system for Mariner-Mars 1964 mission
Mathematical model of Mariner mission success probability
Heat sterilizable power sources for Mariner Mars landing capsule
Combined integrated and discrete circuit breadboard model for redundant multiple logic version of Mariner C spacecraft central computer and sequencer
Scientific results of Mariner II and Mariner IV missions to Mars and Venus, measurements of exospheric structure, and spacecraft systems designs and trajectories
Scientific instrumentation design for 1962 and 1964 Mariner spacecrafts
Estimation of lift-off and transonic vibration spectra on Mariner Mars 1964 spacecraft to enhance survival probability in acoustically induced vibration environment during boost phase
Mission planning and spacecraft development for Mariner Mars project