@rosborne979,
2012 August 7
A Wheel on Mars
Credit: NASA/ JPL-Caltech/Mars Science Laboratory
Explanation: A wheel attached to NASA's Curiosity rover is firmly on the martian surface in this early picture from the Mars Science Laboratory mission, captured after a successful landing on August 5, 2012 at 10:32pm (PDT). Seen at the lower right of a Hazard Avoidance Camera fisheye wide-angle image, the rover's left rear wheel is 50 centimeters (about 20 inches) in diameter. Part of a spring hinge for the camera's dust cover is just visible in the right corner, while at the upper left is part of the rover's RTG power source. Looking into the Sun across the rock stewn surface of Mars, distant hills on the right are the rim of Gale Crater, about 20 kilometers from the compact car-sized rover's current resting place.
PHOTOS
http://photojournal.jpl.nasa.gov/jpegMod/PIA15973_modest.jpg
Original Caption Released with Image:
This is one of the first images taken by NASA's Curiosity rover, which landed on Mars the evening of Aug. 5 PDT (morning of Aug. 6 EDT). It was taken through a "fisheye" wide-angle lens on the left "eye" of a stereo pair of Hazard-Avoidance cameras on the left-rear side of the rover. The image is one-half of full resolution. The clear dust cover that protected the camera during landing has been sprung open. Part of the spring that released the dust cover can be seen at the bottom right, near the rover's wheel.
On the top left, part of the rover's power supply is visible.
Some dust appears on the lens even with the dust cover off.
The cameras are looking directly into the sun, so the top of the image is saturated. Looking straight into the sun does not harm the cameras. The lines across the top are an artifact called "blooming" that occurs in the camera's detector because of the saturation.
As planned, the rover's early engineering images are lower resolution. Larger color images from other cameras are expected later in the week when the rover's mast, carrying high-resolution cameras, is deployed.
Image Credit:
NASA/JPL-Caltech
Image Addition Date:
2012-08-06
PHOTO
Wheels and Legs
The rover's wheels and "legs"
The Mars Science Laboratory has six wheels, each with its own individual motor.
The two front and two rear wheels also have individual steering motors (1 each). This steering capability allows the vehicle to turn in place, a full 360 degrees. The 4-wheel steering also allows the rover to swerve and curve, making arching turns.
How the Wheels Move
Big Wheels Cross The Finish Line...for Now!
Big Wheels Cross The Finish Line...for Now!
One of the black, cleated wheels of the Mars Science Laboratory rover.
The design of the suspension system for the wheels is based on heritage from the "rocker-bogie" system on the Pathfinder and Mars Exploration Rover missions. The suspension system is how the wheels are connected to and interact with the rover body.
The term "bogie" comes from old railroad systems. A bogie is a train undercarriage with six wheels that can swivel to curve along a track.
The term "rocker" comes from the design of the differential, which keeps the rover body balanced, enabling it to "rock" up or down depending on the various positions of the multiple wheels. Of most importance when creating a suspension system is how to prevent the rover from suddenly and dramatically changing positions while cruising over rocky terrain. If one side of the rover were to travel over a rock, the rover body would go out of balance without a "differential" or "rocker," which helps balance the angle the rover is in at any given time. When one side of the rover goes up, the differential or rocker in the rover suspension system automatically makes the other side go down to even out the weight load on the six wheels. This system causes the rover body to go through only half of the range of motion that the "legs" and wheels could potentially experience without a "rocker-bogie" suspension system.
The rover is designed to withstand a tilt of 45 degrees in any direction without overturning. However, the rover is programmed through its "fault protection limits" in its hazard avoidance software to avoid exceeding tilts of 30 degrees during its traverses.
The rover rocker-bogie design allows the rover to go over obstacles (such as rocks) or through holes that are more than a wheel diameter (50 centimeters or about 20 inches) in size. Each wheel also has cleats, providing grip for climbing in soft sand and scrambling over rocks.
Rover Speed
The rover has a top speed on flat hard ground of 4 centimeters per second (a little over 1.5 inches per second).
PHOTO
Power
Power provides electricity to the spacecraft and its subsystems. Below are examples of the way in which the Mars Science Laboratory mission benefits from past technological development and contributes new capabilities.
Inherited Technologies
Mars Science Laboratory uses a radioisotope power system to generate electricity needed to operate the rover and its instruments. Radioisotope electrical power and heating systems enable science missions that require greater longevity, more diverse landing locations or more power or heat than missions limited to solar power systems.
Related Links
Multi-Mission Radioisotope Thermoelectric Generator (MMRTG)
More About Radioisotope Power
Radioisotope power systems are generators that produce electricity from the natural decay of plutonium-238, which is a non-weapons-grade form of that radioisotope used in power systems for NASA spacecraft. Heat given off by the natural decay of this isotope is converted into electricity, providing constant power during all seasons and through the day and night.
Radioisotope power systems were first flown on U.S. space vehicles more than 40 years ago. They offer the key advantage of operating continuously, independent of sunlight, for a long time. They have little or no sensitivity to cold, radiation or other effects of the space environment. More than two dozen NASA spacecraft have conducted their missions using such systems for electrical power and/or heating. For example, the Viking landers, each with a radioisotope thermoelectric generator, landed on Mars in 1976 and operated on Mars for four and six years respectively. The solar-powered 1997 Mars Pathfinder mission's Sojourner rover used radioisotope heaters to keep its electronics box warm. The solar-powered Mars Exploration Rovers Spirit and Opportunity also use radioisotope heaters.
New Capabilities
The need for reliable, long-lived power systems is important for future, increasingly sophisticated Mars missions. NASA and the Department of Energy are developing a new generation of these long-lived, reliable nuclear power systems to enable a broader range of important science missions. They are ideally suited for missions involving autonomous operations in the extreme environments of space and on planetary surfaces.
One of these next-generation space power systems was chosen as the electrical power system for the Mars Science Laboratory -- the Multi-Mission Radioisotope Thermoelectric Generator (MMRTG).
The use of this power source will enable:
Access to More of Mars
This type of power supply will give the mission an operating lifespan on Mars' surface of a full Martian year (687 Earth days, a little less than two Earth years) over a wide latitude range. That means it opens up more regions of Mars to exploration, giving mission planners more choices in selecting landing sites that have characteristics related to Mars' potential as a habitat for life. With more of Mars accessible, Mars Science Laboratory can better meet its science goal of understanding the planet's potential as a past or present habitat for life.
Greater Mobility, More Operational Flexibility, and More Science
Compared to the solar power alternative studied, the MMRTG-powered rover provides significantly greater mobility and operations flexibility and more science payload capability.
Thermal Stability for the Rover
The MMRTG is also crucial for the rover's thermal stability. Waste heat from the unit is circulated throughout the rover system to keep instruments, computers, mechanical devices and communications systems within their operating temperature ranges. This system-wide thermal control does not draw on the rover's electrical power, and precludes the need for radioisotope heater units for spot heating.
Optimized Power and a Long Lifetime
The MMRTG optimizes power levels over a minimum lifetime of 14 years.
Smaller Size and Minimized Weight
With its smaller size, the MMRTG adds more flexibility to spacecraft and mission designs. Compared to the solar power alternative studied, the MMRTG minimizes weight.
Safety
The design requirements of the MMRTG include ensuring a high degree of safety. The design of the generator's General Purpose Heat Source (GPHS) module, which contains the radioisotope heat source, is enhanced and provides added factors of safety in the event of impact or inadvertent reentry.
INFORMATION
2011 July 29
Gale Crater
Credit: NASA, JPL-Caltech, ASU
Explanation: This sharp view from the Thermal Emission Imaging System camera on NASA's Mars Odyssey orbiter is centered on 154 kilometer (96 mile) wide Gale crater, near the martian equator. Within Gale, an impressive layered mountain rises about 5 kilometers (3 miles) above the crater floor. Layers and structures near its base are thought to have been formed in ancient times by water-carried sediments. In fact, a spot near the crater's northern side at the foot of the mountain has now been chosen as the target for the Mars Science Laboratory mission. Scheduled for launch late this year, the mission will land Mars' next visitor from planet Earth in August of 2012, lowering the car-sized Curiosity rover to the martian surface with a hovering, rocket-powered skycrane. Curiosity's science instruments are intended to discover if Gale once had favorable environmental conditions for supporting microbial life and for preserving clues about whether life ever existed on the Red Planet.
PHOTO
http://apod.nasa.gov/apod/image/1107/GaleCraterMars_themis.jpg