TY - JOUR
T1 - AVIATR-Aerial Vehicle for In-situ and Airborne Titan Reconnaissance
AU - Barnes, Jason W.
AU - Lemke, Lawrence
AU - Foch, Rick
AU - McKay, Christopher P.
AU - Beyer, Ross A.
AU - Radebaugh, Jani
AU - Atkinson, David H.
AU - Lorenz, Ralph D.
AU - Le Mouélic, Stéphane
AU - Rodriguez, Sebastien
AU - Gundlach, Jay
AU - Giannini, Francesco
AU - Bain, Sean
AU - Flasar, F. Michael
AU - Hurford, Terry
AU - Anderson, Carrie M.
AU - Merrison, Jon
AU - Ádámkovics, Máté
AU - Kattenhorn, Simon A.
AU - Mitchell, Jonathan
AU - Burr, Devon M.
AU - Colaprete, Anthony
AU - Schaller, Emily
AU - Friedson, A. James
AU - Edgett, Kenneth S.
AU - Coradini, Angioletta
AU - Adriani, Alberto
AU - Sayanagi, Kunio M.
AU - Malaska, Michael J.
AU - Morabito, David
AU - Reh, Kim
N1 - Funding Information:
Acknowledgements The authors acknowledge support from the Idaho Space Grant Consortium, Idaho NASA EPSCoR, the University of Idaho, the University of Idaho College of Engineering, the University of Idaho College of Science, and California Institute of Technology Jet Propulsion Laboratory.
PY - 2012/3
Y1 - 2012/3
N2 - We describe a mission concept for a stand-alone Titan airplane mission: Aerial Vehicle for In-situ and Airborne Titan Reconnaissance (AVIATR). With independent delivery and direct-to-Earth communications, AVIATR could contribute to Titan science either alone or as part of a sustained Titan Exploration Program. As a focused mission, AVIATR as we have envisioned it would concentrate on the science that an airplane can do best: exploration of Titan's global diversity. We focus on surface geology/hydrology and lower-atmospheric structure and dynamics. With a carefully chosen set of seven instruments-2 near-IR cameras, 1 near-IR spectrometer, a RADAR altimeter, an atmospheric structure suite, a haze sensor, and a raindrop detector-AVIATR could accomplish a significant subset of the scientific objectives of the aerial element of flagship studies. The AVIATR spacecraft stack is composed of a Space Vehicle (SV) for cruise, an Entry Vehicle (EV) for entry and descent, and the Air Vehicle (AV) to fly in Titan's atmosphere. Using an Earth-Jupiter gravity assist trajectory delivers the spacecraft to Titan in 7. 5 years, after which the AVIATR AV would operate for a 1-Earth-year nominal mission. We propose a novel 'gravity battery' climb-then-glide strategy to store energy for optimal use during telecommunications sessions. We would optimize our science by using the flexibility of the airplane platform, generating context data and stereo pairs by flying and banking the AV instead of using gimbaled cameras. AVIATR would climb up to 14 km altitude and descend down to 3. 5 km altitude once per Earth day, allowing for repeated atmospheric structure and wind measurements all over the globe. An initial Team-X run at JPL priced the AVIATR mission at FY10 $715M based on the rules stipulated in the recent Discovery announcement of opportunity. Hence we find that a standalone Titan airplane mission can achieve important science building on Cassini's discoveries and can likely do so within a New Frontiers budget.
AB - We describe a mission concept for a stand-alone Titan airplane mission: Aerial Vehicle for In-situ and Airborne Titan Reconnaissance (AVIATR). With independent delivery and direct-to-Earth communications, AVIATR could contribute to Titan science either alone or as part of a sustained Titan Exploration Program. As a focused mission, AVIATR as we have envisioned it would concentrate on the science that an airplane can do best: exploration of Titan's global diversity. We focus on surface geology/hydrology and lower-atmospheric structure and dynamics. With a carefully chosen set of seven instruments-2 near-IR cameras, 1 near-IR spectrometer, a RADAR altimeter, an atmospheric structure suite, a haze sensor, and a raindrop detector-AVIATR could accomplish a significant subset of the scientific objectives of the aerial element of flagship studies. The AVIATR spacecraft stack is composed of a Space Vehicle (SV) for cruise, an Entry Vehicle (EV) for entry and descent, and the Air Vehicle (AV) to fly in Titan's atmosphere. Using an Earth-Jupiter gravity assist trajectory delivers the spacecraft to Titan in 7. 5 years, after which the AVIATR AV would operate for a 1-Earth-year nominal mission. We propose a novel 'gravity battery' climb-then-glide strategy to store energy for optimal use during telecommunications sessions. We would optimize our science by using the flexibility of the airplane platform, generating context data and stereo pairs by flying and banking the AV instead of using gimbaled cameras. AVIATR would climb up to 14 km altitude and descend down to 3. 5 km altitude once per Earth day, allowing for repeated atmospheric structure and wind measurements all over the globe. An initial Team-X run at JPL priced the AVIATR mission at FY10 $715M based on the rules stipulated in the recent Discovery announcement of opportunity. Hence we find that a standalone Titan airplane mission can achieve important science building on Cassini's discoveries and can likely do so within a New Frontiers budget.
KW - Airplane
KW - Mission concept
KW - Titan
KW - UAV
UR - http://www.scopus.com/inward/record.url?scp=84857912609&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84857912609&partnerID=8YFLogxK
U2 - 10.1007/s10686-011-9275-9
DO - 10.1007/s10686-011-9275-9
M3 - Article
AN - SCOPUS:84857912609
SN - 0922-6435
VL - 33
SP - 55
EP - 127
JO - Experimental Astronomy
JF - Experimental Astronomy
IS - 1
ER -