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Scientific and Technical Aerospace Reports Volume 38 July 28, 2000

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major limitations: 1) Only a limited number of rocks were viewed by the rover, biasing flute statistics; <strong>and</strong> 2) The higher resolution<br />

obtained by the rover images <strong>and</strong> the lack of such pictures at the Viking l<strong>and</strong>ing sites hampered comparisons of rock morphologies<br />

between the Pathfinder <strong>and</strong> Viking sites. to avoid this problem, rock morphology <strong>and</strong> ventifact statistics have been examined using<br />

new ”super-resolution” IMP <strong>and</strong> Viking L<strong>and</strong>er images. Analyses of these images show that: 1) Flutes are seen on about 50% or<br />

more of the rocks in the near field at the MPF site; 2) The orientation of these flutes is similar to that for flutes identified in rover<br />

images; <strong>and</strong> 3) Ventifacts are significantly more abundant at the Pathfinder l<strong>and</strong>ing site than at the two Viking L<strong>and</strong>ing sites, where<br />

rocks have undergone only a limited amount of aeolian abrasion. This is most likely due to the ruggedness of the Pathfinder site<br />

<strong>and</strong> a greater supply of abrading particles available shortly after the Arcs <strong>and</strong> Tiu Valles outflow channel floods.<br />

Derived from text<br />

L<strong>and</strong>ing Sites; Abrasion; Rocks; Mars Pathfinder; Mars Surface<br />

<strong>2000</strong>0062727 NASA Kennedy Space Center, Cocoa Beach, FL USA<br />

TITAN III Launch Replays<br />

Sep. 25, 1992; In English; Videotape: 9 min. playing time, in color, without sound<br />

Report No.(s): NONP-NASA-VT-<strong>2000</strong>081549; No Copyright; Avail: CASI; B01, Videotape-Beta; V01, Videotape-VHS<br />

Footage shows several views of the launching of the Mars Observer Titan III satellite. Scenes include different angle <strong>and</strong><br />

camera views of the launch. Also shown are panoramic views of the launch vehicle on the launch pad.<br />

CASI<br />

Titan; Launch Vehicles; Titan Project; Mars Observer; Launching<br />

<strong>2000</strong>0063<strong>38</strong>4 NASA Kennedy Space Center, Cocoa Beach, FL USA<br />

Mars Observer Press Conference JPL<br />

Aug. 24, 1993; In English; Videotape: 55 min. 1 sec. playing time, in color, with sound<br />

Report No.(s): NONP-NASA-VT-<strong>2000</strong>81550; No Copyright; Avail: CASI; B03, Videotape-Beta; V03, Videotape-VHS<br />

The Mars Observer mission spacecraft was primarily designed for exploring Mars <strong>and</strong> the Martian environment. The Mars<br />

Observer was launched on September 25, 1992. The spacecraft was lost in the vicinity of Mars on August 21, 1993 when the spacecraft<br />

began its maneuvering sequence for Martian orbital insertion. This videotape shows a press briefing, held after the spacecraft<br />

had not responded to attempts to communicate with it, to explain to the press the problems <strong>and</strong> the steps that were being taken<br />

to re-establish communication with the spacecraft. The communications had been shutdown prior to the orbital insertion burn to<br />

protect the instruments. At the time of the press conference, the communications system was still not operational, <strong>and</strong> attempts<br />

were being made to re-establish communication. Bob McMillan of the Public Affairs Office at JPL gives the initial announcement<br />

of the continuing communication problem with the spacecraft. Mr. McMillan introduces William Piotrowski, acting director of<br />

solar system exploration, who reiterates that there is indeed no communication with the Observer spacecraft. He is followed by<br />

Glenn Cunningham, the Project Manager of the Mars Observer who speaks about the attempts to re-establish contact. Mr. Cunningham<br />

is followed by Satenios Dallas, the Mission Manager for the Mars Observer Project, who speaks about the sequence of<br />

events leading up to the communication failure, <strong>and</strong> shows an animated video presenting the orbital insertion maneuvers. The<br />

briefing was then opened up for questions from the assembled press, both at JPL <strong>and</strong> at the other NASA Centers. The questions<br />

are about the possible reasons for the communication failure, <strong>and</strong> the attempts to restore communications with the spacecraft. Dr.<br />

Arden L. Albee, chief scientist for the Mars Observer Mission, joins the other panel members to answer questions. At the end of<br />

the press briefing the animation of the Mars orbital insertion is shown again.<br />

CASI<br />

Failure; Orbit Insertion; Mars Probes; Mars Missions<br />

<strong>2000</strong>0063<strong>38</strong>5 NASA Kennedy Space Center, Cocoa Beach, FL USA<br />

Mars Observer Lecture: Mars Orbit Insertion<br />

Dodd, Suzanne R., Personal Name; Aug. 17, 1993; In English; Videotape: 45 min. 45 sec. playing time, in color, with sound<br />

Report No.(s): NONP-NASA-VT-<strong>2000</strong>0815<strong>38</strong>; No Copyright; Avail: CASI; B03, Videotape-Beta; V03, Videotape-VHS<br />

The Mars Observer mission spacecraft was primarily designed for exploring Mars <strong>and</strong> the Martian environment. The Mars<br />

Observer was launched on September 25, 1992. The spacecraft was lost in the vicinity of Mars on August 21, 1993 when the spacecraft<br />

began its maneuvering sequence for Martian orbital insertion. This videotape shows a lecture by Suzanne R. Dodd, the Mission<br />

Planning Team Chief for the Mars Observer Project. Ms Dodd begins with a brief overview of the mission <strong>and</strong> the timeline<br />

from the launch to orbital insertion. Ms Dodd then reviews slides showing the trajectory of the spacecraft on its trip to Mars. Slides<br />

of the spacecraft being constructed are also shown. She then discusses the Mars orbit insertion <strong>and</strong> the events that will occur to<br />

move the spacecraft from the capture orbit into a mapping orbit. During the trip to Mars, scientists at JPL had devised a new strat-<br />

2<strong>28</strong>

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