TY - JOUR
T1 - The OSIRIS-REx Spacecraft and the Touch-and-Go Sample Acquisition Mechanism (TAGSAM)
AU - the OSIRIS-REx Team
AU - Bierhaus, E. B.
AU - Clark, B. C.
AU - Harris, J. W.
AU - Payne, K. S.
AU - Dubisher, R. D.
AU - Wurts, D. W.
AU - Hund, R. A.
AU - Kuhns, R. M.
AU - Linn, T. M.
AU - Wood, J. L.
AU - May, A. J.
AU - Dworkin, J. P.
AU - Beshore, E.
AU - Lauretta, D. S.
N1 - Funding Information:
We thank the many people whose hard work, dedication, and passion for this mission transformed an idea into a spacecraft en route to Bennu. This work was supported by National Aeronautics and Space Administration contract NNG12FD66C. The October 2012 test campaign was an excellent series of tests, as the pilots enabled our fundamental test objective to perform collection tests in a small but always positive acceleration environment. We offer thanks to NASA’s RGO and the pilots for meeting our unique requirements, and for their incredible support during the week. The data collected during those flights are fundamental contributions to our understanding of TAGSAM performance at Bennu. OSIRIS-REx Edited by Dante Lauretta and Christopher T. Russell B.C. Clark, R.A. Hund and E. Beshore are retired.
Publisher Copyright:
© 2018, The Author(s).
PY - 2018/10/1
Y1 - 2018/10/1
N2 - The Origins, Spectral-Interpretation, Resource-Identification, Security and Regolith-Explorer (OSIRIS-REx) spacecraft supports all aspects of the mission science objectives, from extensive remote sensing at the asteroid Bennu, to sample collection and return to Earth. In general, the success of planetary missions requires the collection, return, and analysis of data, which in turn depends on the successful operation of instruments and the host spacecraft. In the case of OSIRIS-REx, a sample-return mission, the spacecraft must also support the acquisition, safe stowage, and return of the sample. The target asteroid is Bennu, a B-class near-Earth asteroid roughly 500 m diameter. The Lockheed Martin-designed and developed OSIRIS-REx spacecraft draws significant heritage from previous missions and features the Touch-and-Go-Sample-Acquisition-Mechanism, or TAGSAM, to collect sample from the surface of Bennu. Lockheed Martin developed TAGSAM as a novel, simple way to collect samples on planetary bodies. During short contact with the asteroid surface, TAGSAM releases curation-grade nitrogen gas, mobilizing the surface regolith into a collection chamber. The contact surface of TAGSAM includes “contact pads”, which are present to collect surface grains that have been subject to space weathering. Extensive 1-g laboratory testing, “reduced-gravity” testing (via parabolic flights on an airplane), and analysis demonstrate that TAGSAM will collect asteroid material in nominal conditions, and a variety of off-nominal conditions, such as the presence of large obstacles under the TAGSAM sampling head, or failure in the sampling gas firing. TAGSAM, and the spacecraft support of the instruments, are central to the success of the mission.
AB - The Origins, Spectral-Interpretation, Resource-Identification, Security and Regolith-Explorer (OSIRIS-REx) spacecraft supports all aspects of the mission science objectives, from extensive remote sensing at the asteroid Bennu, to sample collection and return to Earth. In general, the success of planetary missions requires the collection, return, and analysis of data, which in turn depends on the successful operation of instruments and the host spacecraft. In the case of OSIRIS-REx, a sample-return mission, the spacecraft must also support the acquisition, safe stowage, and return of the sample. The target asteroid is Bennu, a B-class near-Earth asteroid roughly 500 m diameter. The Lockheed Martin-designed and developed OSIRIS-REx spacecraft draws significant heritage from previous missions and features the Touch-and-Go-Sample-Acquisition-Mechanism, or TAGSAM, to collect sample from the surface of Bennu. Lockheed Martin developed TAGSAM as a novel, simple way to collect samples on planetary bodies. During short contact with the asteroid surface, TAGSAM releases curation-grade nitrogen gas, mobilizing the surface regolith into a collection chamber. The contact surface of TAGSAM includes “contact pads”, which are present to collect surface grains that have been subject to space weathering. Extensive 1-g laboratory testing, “reduced-gravity” testing (via parabolic flights on an airplane), and analysis demonstrate that TAGSAM will collect asteroid material in nominal conditions, and a variety of off-nominal conditions, such as the presence of large obstacles under the TAGSAM sampling head, or failure in the sampling gas firing. TAGSAM, and the spacecraft support of the instruments, are central to the success of the mission.
KW - Asteroid
KW - Bennu
KW - OSIRIS-REx
KW - Spacecraft
KW - TAGSAM
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U2 - 10.1007/s11214-018-0521-6
DO - 10.1007/s11214-018-0521-6
M3 - Review article
AN - SCOPUS:85053609063
SN - 0038-6308
VL - 214
JO - Space Science Reviews
JF - Space Science Reviews
IS - 7
M1 - 107
ER -