Lunar surface thermal-characteristics during eclipse from Surveyors III, V and after sunset from Surveyor V.
Lunar surface thermal characteristics during eclipse from Surveyors 3, 5 and after sunset from Surveyor 5
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Lunar surface thermal characteristics during eclipse from Surveyors 3, 5 and after sunset from Surveyor 5
One of the original objectives of the Mars Orbiter Camera (MOC), as proposed in 1985, was to acquire observations to be used in assessing future spacecraft landing sites. Images obtained by the Mars Global Surveyor MOC since March 1999 provide the highest resolution views (1.5-4.5 m/pixel) of the planet ever seen. We have been examining these new data to develop a general view of what Mars is like at meter-scale within the latitudes and elevations that are accessible to the Mars Surveyor 2001 lander. Our goal is to provide guidance to the 2001 landing site selection process, rather than to use MOC images to recommend a specific landing site.
Engineering analyses on Surveyor lunar dust particle detector instrumentation, and ground support equipment
Dynamic behavior of Surveyor landing system and surface material during lunar landing
Data processing systems, thermal subsystems, design, and mission performance summary for Surveyor 1 spacecraft
Performance analysis of electric power, data link, signal processing, and flight control systems of Surveyor 1 spacecraft
Performance analysis of propulsion system, retrorocket, altitude radar, radar altimeter, and television system of Surveyor 1 spacecraft
Flight performance characteristics of Surveyor 2 spacecraft and its subsystems
Real time and postflight data used for reporting flight performance characteristics of Surveyor 3 spacecraft and its subsystems, including TV equipment and soil mechanics/surface sampler
Flight performance of Surveyor 4 spacecraft and subsystems analyses data
Flight performance analysis of Surveyor 5 spacecraft, including TV equipment and alpha scattering device data
Surveyor 6 spacecraft flight performance characteristics, including data on television equipment, alpha scattering experiment, and powered flight translation
Surveyor Mission G flight operations from transit phase to second lunar day
Surveyor 1 and 2 trajectories determined from tracking data
Surveyor 3 and 4 spacecraft flight paths
Performance analyses of Surveyor 7 lunar probe including launch, orbit, descent, photography, alpha scattering measurements, and soil sampling
Surveyor 5, 6, 7 missions alpha-scattering experiments, lunar rocks chemical composition compared with earth rocks and chondritic meteorites
Near the eastern shore of Oceanus Procellarum, 390 miles from Surveyor I, stands Surveyor III, now motionless and silent after a full lunar day's work during which the spacecraft transmitted to Earth 6315 photographs of its surroundings. A surface sampler, operated by command from the Earth and in view of Surveyor's television camera, conducted many tests of the character and structure of the lunar surface material, as well as digging four trenches. While Surveyor I put man's eyes on the Moon, Surveyor III added an arm and a hand with which to work. In this mission, Surveyor displayed remarkable adaptability and stability. Because the engines did not cut off before touchdown, the spacecraft in effect made three separate landings, giving information on surface bearing strength in several places. The spacecraft came to rest at an angle of about 14° from the vertical, well below the rim of a crater, making possible a detailed study of the floor and walls of a small lunar crater. The tilted position of the spacecraft also made it possible to obtain, for the first time from the surface of the Moon, photographs of a solar eclipse, and of the Earth in color. This report presents the preliminary findings from Surveyor III of the team of scientists and engineers of the Surveyor Program.