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Icarus | 1972

Variable features on Mars: Preliminary mariner 9 television results

Carl Sagan; Joseph Veverka; P. Fox; Russell Dubisch; Joshua Lederberg; Elliott C. Levinthal; Lynn Quam; R. B. Tucker; James B. Pollack; Bradford A. Smith

Abstract Systematic Mariner 9 photography of a range of Martian surface features, observed with all three photometric angles approximately invariant, reveals three general categories of albedo variations: (1) an essentially uniform contrast enhancement due to the dissipation of the dust storm; (2) the appearance of splotches, irregular dark markings at least partially related to topography; and (3) the development of both bright and dark linear streaks, generally emanating from craters. Some splotches and streaks vary on characteristic timescales ∼2 weeks; they have characteristic dimensions of kilometers to tens of kilometers. The loci of these features appear in some cases to correspond well to the ground-based albedo markings, and the integrated time variation of splotches and streaks is suggested to produce the classical “seasonal” and secular albedo changes on Mars. The morphology and variability of streaks and splotches, and the resolution of at least one splotch into an extensive dune system, implicates windblown dust as the principal agent of Martian albedo differences and variability.


Science | 1976

The Surface of Mars: The View from the Viking 2 Lander

Thomas A. Mutch; Alan B. Binder; Friedrich O. Huck; Elliott C. Levinthal; Sidney Liebes; Elliot C. Morris; William R. Patterson; James B. Pollack; Carl Sagan; Glenn R. Taylor

Viking 2 lander began imaging the surface of Mars at Utopia Planitia on 3 September 1976. The surface is a boulder-strewn reddish desert cut by troughs that probably form a polygonal network. A plateau can be seen to the east of the spacecraft, which for the most probable lander location is approximately the direction of a tongue of ejecta from the crater Mie. Boulders at the lander 2 site are generally more vesicular than those near lander i. Fines at both lander sites appear to be very fine-grained and to be bound in a duricrust. The pinkish color of the sky, similar to that observed at the lander I site, indicates suspension of surface material. However, the atmospheric optical depth is less than that at the lander I site. After dissipation of a cloud of dust stirred during landing, no changes other than those stemming from sampling activities have been detected in the landscape. No signs of large organisms are apparent at either landing site.


Science | 1972

Mariner 9 television reconnaissance of Mars and its satellites: Preliminary results

Harold Masursky; Raymond M. Batson; John F. McCauley; L. A. Soderblom; Robert L. Wildey; Michael H. Carr; Daniel J. Milton; Don E. Wilhelms; Bradford A. Smith; T. B. Kirby; J.C. Robinson; Conway B. Leovy; G. Briggs; T. C. Duxbury; C. H. Acton; Bruce C. Murray; James A. Cutts; Robert P. Sharp; Susan Smith; Robert B. Leighton; Carl Sagan; Joseph Veverka; M. Noland; Joshua Lederberg; Elliott C. Levinthal; J. B. Pollack; J. T. Moore; William K. Hartmann; E. Shipley; G. de Vaucouleurs

At orbit insertion on 14 November 1971 the Martian surface was largely obscured by a dust haze with an extinction optical depth that ranged from near unity in the south polar region to probably greater than 2 over most of the planet. The only features clearly visible were the south polar cap, one dark, spot in Nix Olympica, and three dark spots in the Tharsis region. During the third week the atmosphere began to clear and surface visibility improved, but contrasts remained a fraction of their normal value. Each of the dark spots that apparently protrude through most of the dust-filled atmosphere has a crater or crater complex in its center. The craters are rimless and have featureless floors that, in the crater complexes, are at different levels. The largest crater within the southernmost spot is approximately 100 kilometers wide. The craters apparently were formed by subsidence and resemble terrestrial calderas. The south polar cap has a regular margin, suggsting very flat topography. Two craters outside the cap have frost on their floors; an apparent crater rim within the cap is frost free, indicating preferentia loss of frost from elevated ground. If this is so then the curvilinear streaks, which were frost covered in 1969 and are now clear of frost, may be low-relief ridges. Closeup pictures of Phobos and Deimos show that Phobos is about 25 �5 by 21 �1 kilometers and Deimos is about 13.5 � 2 by 12.0 �0.5 kilometers. Both have irregular shapes and are highly cratered, with some craters showing raised rims. The satellites are dark objects with geometric albedos of 0.05.


Science | 1976

The surface of Mars: there view from the viking 1 lander.

Thomas A. Mutch; Alan B. Binder; Friedrich O. Huck; Elliott C. Levinthal; Sidney Liebes; Elliot C. Morris; William R. Patterson; James B. Pollack; Carl Sagan; Glenn R. Taylor

The first photographs ever returned from the surface of Mars were obtained by two facsimile cameras aboard the Viking 1 lander, including black-and-white and color, 0.12� and 0.04� resolution, and monoscopic and stereoscopic images. The surface, on the western slopes of Chtyse Planitia, is a boulder-strewn deeply reddish desert, with distant eminences—some of which may be the rims of impact craters—surmounted by a pink sky. Both impact and aeolian processes are evident. After dissipation of a small dust cloud stirred by the landing maneuvers, no subsequent signs of movement were detected on the landscape, and nothing has been observed that is indicative of macroscopic biology at this time and place.


Science | 1976

Fine Particles on Mars: Observations with the Viking 1 Lander Cameras

Thomas A. Mutch; Raymond E. Arvidson; Alan B. Binder; Friedrich O. Huck; Elliott C. Levinthal; Sidney Liebes; Elliot C. Morris; Dag Nummedal; James B. Pollack; Carl Sagan

Drifts of fine-grained sediment are present in the vicinity of the Viking 1 lander. Many drifts occur in the lees of large boulders. Morphologic analysis indicates that the last dynamic event was one of general deflation for at least some drifts. Particle cohesion implies that there is a distinct small-particle upturn in the threshold velocity-particle size curve; the apparent absence of the most easily moved particles (150 micrometers in diameter) may be due to their preferential transport to other regions or their preferential collisional destruction. A twilight rescan with lander cameras indicates a substantial amount of red dust with mean radius on the order of 1 micrometer in the atmosphere.


Icarus | 1972

Imaging experiment: The Viking Lander

Thomas A. Mutch; Alan B. Binder; Friedrich O. Huck; Elliott C. Levinthal; Elliot C. Morris; Carl Sagan; A.T. Young

Abstract The Viking Lander Imaging System will consist of two identical facsimile cameras. Each camera has a high-resolution mode with an instantaneous field of view of 0.04°, and survey and color modes with instantaneous fields of view of 0.12°. Cameras are positioned one meter apart to provide stereoscopic coverage of the near-field. The Imaging Experiment will provide important information about the morphology, composition, and origin of the Martian surface and atmospheric features. In addition, lander pictures will provide supporting information for other experiments in biology, organic chemistry, meteorology, and physical properties.


Icarus | 1970

Television experiment for Mariner Mars 1971

Harold Masursky; Raymond M. Batson; W. Borgeson; Michael H. Carr; John F. McCauley; Daniel J. Milton; Robert L. Wildey; Don E. Wilhelms; Bruce C. Murray; Norman H. Horowitz; Robert B. Leighton; Robert P. Sharp; W. Thompson; G. Briggs; P. Chandeysson; E. Shipley; Carl Sagan; James B. Pollack; Joshua Lederberg; Elliott C. Levinthal; William K. Hartmann; Thomas B. McCord; Bradford A. Smith; Merton E. Davies; G. de Vaucouleurs; Conway B. Leovy

Abstract The Television Experiment objectives are to provide imaging data which will complement previously gathered data and extend our knowledge of Mars. The two types of investigations will be fixed-feature (for mapping) and variable-feature (for surface and atmospheric changes). Two cameras with a factor-of-ten difference in resolution will be used on each spacecraft for medium- and high-resolution imagery. Mapping of 70% of the planets surface will be provided by medium-resolution imagery. Spot coverage of about 5% of the surface will be possible with the high-resolution imagery. The experiments 5 Principal Investigators and 21 Co-Investigators are organized into a team. Scientific disciplines and technical task groups have been formed to provide the formulation of experiment requirements for mission planning and instrument development. It is expected that the team concept will continue through the operational and reporting phases of the Mariner Mars 1971 Project.


Icarus | 1973

Mariner 9 - Image processing and products.

Elliott C. Levinthal; W.B. Green; James A. Cutts; E.D. Jahelka; R.A. Johansen; M.J. Sander; J.B. Seidman; A.T. Young; L. A. Soderblom

Abstract The purpose of this paper is to describe the system for the display, processing, and production of image-data products created to support the Mariner 9 Television Experiment. Of necessity, the system was large in order to respond to the needs of a large team of scientists with a broad scope of experimental objectives. The desire to generate processed data products as rapidly as possible to take advantage of adaptive planning during the mission, coupled with the complexities introduced by the nature of the vidicon camera, greatly increased the scale of the ground-image processing effort. This paper describes the systems that carried out the processes and delivered the products necessary for real-time and near-real-time analyses. References are made to the computer algorithms used for the, different levels of decalibration and analysis.


A New Era in Space Transportation#R##N#Proceedings of the XXVIIth International Astronautical Congress, Anaheim, 10–16 October 1976 | 1976

MULTISPECTRAL AND STEREO IMAGING ON MARS

Elliott C. Levinthal; Friedrich O. Huck

Relevant aspects of the design and function of the two-window Viking Landing Camera system are described, with particular reference to some results of its operation on Mars during the Viking mission. A major feature of the system is that the optical tunnel between the lens and the photosensor array contains a multiaperture baffle designed to reduce veiling glare and to attenuate radio frequency interference from the lander antennas. The principle of operation of the contour mode is described. The accuracy is limited by the stereo base, resolution of camera picture elements, and geometric calibration. To help determine the desirability as well as the safety of possible sample sites, use is made of both radiometric and photogrammetric information for each picture element to combine high-resolution pictures with low-resolution color pictures of the same area. Explanatory photographs supplement the text.


Proceedings of the 1974 annual ACM conference on | 1974

SUMEX: a resource for applications of artificial intelligence in medicine

Joshua Lederberg; Edward A. Feigenbaum; Elliott C. Levinthal; Thomas C. Rindfleisch

In partnership with the Biotechnology Resources Branch (BRB) of the Division of Research Resources of the National Institutes of Health, Stanford University is developing a nationally shared computing resource to promote research in artificial intelligence (AI) oriented to bio-medical problems. Based on an initial national community of projects and taking advantage of current data communications technologies, the SUMEX (Stanford University Medical Experimental Computer) project hopes to provide an efficient engineering support team and software library for such investigations, and to promote a more systematic exchange of research tools, products, and ideas among existing projects.

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Bruce C. Murray

California Institute of Technology

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Daniel J. Milton

United States Geological Survey

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