Other
Scientific paper
Jan 2006
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006aipc..813..356a&link_type=abstract
SPACE TECH.& APPLIC.INT.FORUM-STAIF 2006: 10th Conf Thermophys Applic Microgravity; 23rd Symp Space Nucl Pwr & Propulsion; 4th C
Other
Thermoelectric, Electrogasdynamic And Other Direct Energy Conversion, Heat Engines, Heat Pumps, Heat Pipes, Spaceborne And Space Research Instruments, Apparatus, And Components, Titan
Scientific paper
With the remarkable success of the Cassini-Huygens mission, considerable new knowledge has been obtained regarding the surface topography, composition and atmospheric characteristics of Titan. However, Cassini-Huygens represents only a bold beginning for the exploration of Titan, as high resolution mapping will have been performed for only a small fraction of the surface of Titan by the end of the nominal mission. Large gaps in knowledge will remain in key scientific areas including global surface topography, atmospheric and surface composition, precipitation rates, and the density, thickness, and formation processes of clouds. This study details a conceptual follow-on Titan orbiter mission that would provide full global topographic coverage, surface imaging, and meteorological characterization of the atmosphere over a nominal 2-year science mission duration. The reference power requirement is ~1 kWe at EOM and is driven by a high power radar instrument that would provide 3-dimensional measurements of atmospheric clouds, precipitation, and surface topography. While this power level is moderately higher than that of the Cassini spacecraft, higher efficiency advanced RPSs could potentially reduce the plutonium usage to less than 1/3 of that used on the Cassini spacecraft. The Titan Orbiter mission is assumed to launch in 2015. It would utilize advanced RPSs to provide all on-board power, and would employ an aeroshell to aerocapture into Titan orbit. A conceptual advanced Stirling RPS was selected due to its high specific power and conversion efficiency which enabled the ability to include a 500 kg ``black box'' deployed entry probe.
Abelson Robert Dean
Shirley James H.
Spilker Thomas Richard
No associations
LandOfFree
A Conceptual Titan Orbiter with Probe Mission Using Advanced Radioisotope Power Systems does not yet have a rating. At this time, there are no reviews or comments for this scientific paper.
If you have personal experience with A Conceptual Titan Orbiter with Probe Mission Using Advanced Radioisotope Power Systems, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and A Conceptual Titan Orbiter with Probe Mission Using Advanced Radioisotope Power Systems will most certainly appreciate the feedback.
Profile ID: LFWR-SCP-O-1283175