Bibcode
Barucci, Maria Antonietta; Cheng, A. F.; Michel, P.; Benner, L. A. M.; Binzel, R. P.; Bland, P. A.; Böhnhardt, H.; Brucato, J. R.; Campo Bagatin, A.; Cerroni, P.; Dotto, E.; Fitzsimmons, A.; Franchi, I. A.; Green, S. F.; Lara, L.-M.; Licandro, J.; Marty, B.; Muinonen, K.; Nathues, A.; Oberst, J.; Rivkin, A. S.; Robert, F.; Saladino, R.; Trigo-Rodriguez, J. M.; Ulamec, S.; Zolensky, M.
Bibliographical reference
Experimental Astronomy, Volume 33, Issue 2-3, pp. 645-684
Advertised on:
4
2012
Journal
Citations
66
Refereed citations
59
Description
MarcoPolo-R is a sample return mission to a primitive Near-Earth
Asteroid (NEA) proposed in collaboration with NASA. It will rendezvous
with a primitive NEA, scientifically characterize it at multiple scales,
and return a unique sample to Earth unaltered by the atmospheric entry
process or terrestrial weathering. MarcoPolo-R will return bulk samples
(up to 2 kg) from an organic-rich binary asteroid to Earth for
laboratory analyses, allowing us to: explore the origin of planetary
materials and initial stages of habitable planet formation; identify and
characterize the organics and volatiles in a primitive asteroid;
understand the unique geomorphology, dynamics and evolution of a binary
NEA. This project is based on the previous Marco Polo mission study,
which was selected for the Assessment Phase of the first round of Cosmic
Vision. Its scientific rationale was highly ranked by ESA committees and
it was not selected only because the estimated cost was higher than the
allotted amount for an M class mission. The cost of MarcoPolo-R will be
reduced to within the ESA medium mission budget by collaboration with
APL (John Hopkins University) and JPL in the NASA program for
coordination with ESA's Cosmic Vision Call. The baseline target is a
binary asteroid (175706) 1996 FG3, which offers a very efficient
operational and technical mission profile. A binary target also provides
enhanced science return. The choice of this target will allow new
investigations to be performed more easily than at a single object, and
also enables investigations of the fascinating geology and geophysics of
asteroids that are impossible at a single object. Several launch windows
have been identified in the time-span 2020-2024. A number of other
possible primitive single targets of high scientific interest have been
identified covering a wide range of possible launch dates. The baseline
mission scenario of MarcoPolo-R to 1996 FG3 is as follows: a single
primary spacecraft provided by ESA, carrying the Earth Re-entry Capsule,
sample acquisition and transfer system provided by NASA, will be
launched by a Soyuz-Fregat rocket from Kourou into GTO and using two
space segment stages. Two similar missions with two launch windows, in
2021 and 2022 and for both sample return in 2029 (with mission duration
of 7 and 8 years), have been defined. Earlier or later launches, in 2020
or 2024, also offer good opportunities. All manoeuvres are carried out
by a chemical propulsion system. MarcoPolo-R takes advantage of three
industrial studies completed as part of the previous Marco Polo mission
(see ESA/SRE (2009)3, Marco Polo Yellow Book) and of the expertise of
the consortium led by Dr. A.F. Cheng (PI of the NASA NEAR Shoemaker
mission) of the JHU-APL, including JPL, NASA ARC, NASA LaRC, and MIT.
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