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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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1,060 records · Page 59

The Pathfinder Microrover

An exciting scientific component of the Pathfinder mission is the rover, which will act as a mini-field geologist by providing us with access to samples for chemical analyses and close-up images of the Martian surface, performing active experiments to modify the surface and study the results, and exploring the landing site area.

Mars Mars Pathfinder rover microrover imager for p↗

Dynamic Model Investigation of the Rough-Water Landing Characteristics of a Spacecraft

The investigation was made to study the rough-water landing characteristics of a Gemini type of spacecraft. The investigations were made with a 1/6-scale dynamic model in a simulated sea state 4 rough water. Parachute letdown landings were simulated with the model at various yaw angles and horizontal velocities. The vertical velocity and landing attitude remained constant. The range of maximum lateral and longitudinal acceleration was from about 3-1/2g to 16g while that for the maximum normal acceleration was from lg to 15g. The range of maximum angular acceleration was from about 0 to 190 radians per second(exp 2). The smoothest behavior and the lowest angular acceleration occurred at the 90 degree yaw angle. The normal acceleration was near minimum at this condition.

[Division] Imp. Str↗

Ulysses Observations of Latitude Gradients in the Heliospheric Magnetic Field

Several parameters measured by Ulysses as it traveled southward to heliographic latitudes of -50° are presented and analyzed. Three topics of scientific importance are investigated: (1) latitude gradient; (2) extent of agreement between observed and Parker spiral angles near -50°; (3) field variances and their interpretation.

Ulysses↗