Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Keith Novak"'
Publikováno v:
Journal of Thermophysics and Heat Transfer. 31:841-846
A literature review of static ball bearing thermal conductance in both air and vacuum was performed, with an emphasis on understanding the conductance that would be expected across ball bearings of...
Publikováno v:
43rd International Conference on Environmental Systems.
On November 26, 2011, NASA launched a large (900 kg) rover as part of the Mars Science Laboratory (MSL) mission to Mars. Eight months later, on August 5, 2012, the MSL rover (Curiosity) successfully touched down on the surface of Mars. As of the writ
In-Flight Performance of the Mars Science Laboratory Spacecraft Cruise Phase Thermal Control Systems
Publikováno v:
42nd International Conference on Environmental Systems.
The National Aeronautics and Space Administration’s Mars Science Laboratory (MSL) mission will land a robotic rover on the surface of Mars for a two-year exploration mission. During the deep space transit from Earth to Mars, the rover will reside i
Publikováno v:
42nd International Conference on Environmental Systems.
On November 26, 2011, NASA launched a large (900 kg) rover as part of the Mars Science Laboratory (MSL) mission to Mars. The MSL rover is scheduled to land on Mars on August 5, 2012. Prior to launch, the Rover was successfully operated in simulated m
Publikováno v:
41st International Conference on Environmental Systems.
The National Aeronautics and Space Administration (NASA) is sending a large (>850 kg) rover as part of the Mars Science Laboratory (MSL) mission to Mars in 2011. The rover's primary power source is a Multi-Mission Radioisotope Thermoelectric Generato
Autor:
M. Prina, Pradeep Bhandari, Brenda Ramirez, David Bame, Keith Novak, Anthony D. Paris, Gajanana C. Birur, Michael Pauken
Publikováno v:
SAE Technical Paper Series.
The Mars Science Laboratory (MSL) mission to land a large rover on Mars is being planned for launch in 2009. This paper will describe the basic architecture of the thermal control system, the challenges and the methods used to overcome them by the us
Publikováno v:
SAE Technical Paper Series.
NASA launched two rovers in June and July of 2003 as a part of the Mars Exploration Rover (MER) project. MER-A (Spirit) landed on Mars in Gusev Crater at 15 degrees South latitude and 175 degree East longitude on January 4, 2004 (Squyres, et al., Dec
Publikováno v:
SAE Technical Paper Series.
The Mars Exploration Rovers (MER), were launched in June and July of 2003, repsectively and successfully landed on Mars in early and late January of 2004, repectively. The flight system architecture implemented many successful features of the Mars Pa
Publikováno v:
SAE Technical Paper Series.
In January 2004, two Mars Exploration Rovers (MER) landed on the surface of Mars to begin their mission as robotic geologists. A year prior to these historic landings, both rovers and the spacecraft that delivered them to Mars, were completing a seri
Publikováno v:
SAE Technical Paper Series.
The viewgraph presentation examines propulsion line heater design and problems in the Mars Rover. Topics include a Mars Exploration Rover (MER) project description and MER spacecraft configuration, mission overview, MER cruise stage hardware, thermal