Technical Papers
Sep 22, 2016

Implications of Sample Size for the Thermal Extraction of Volatiles from Lunar Regolith with the PROSPECT Instrument Package

Publication: Journal of Aerospace Engineering
Volume 30, Issue 3

Abstract

The platform for resource observation and in situ prospecting for exploration, commercial exploitation, and transportation (PROSPECT) instrument package is under development by the European Space Agency for the upcoming Luna-27 mission to the lunar south pole. The purpose of the instrument is to detect and quantify volatiles on the lunar surface with the processing and analysis unit ProSPA. This paper describes the feasibility study and early breadboarding activities on ProSPA sample ovens during the Phase A study. The review of similar sample oven concepts led to the conclusion that none of these concepts satisfies new requirements of ProSPA regarding sample size and target temperatures. The trade studies presented in this paper include the estimation of power demands for scaled-up ovens, the influence of oven insulation, the compatibility of the utilized materials, and an experimental validation of the design. Experimental tests showed that the new oven design allows reaching the target temperatures and following most of the specified heating profiles with an imposed maximum power of 70 W. During the heating tests with the lunar regolith simulant NU-LHT-2M, sintering of the sample, reduction of the FeO content, and the creation of gas cavities were observed.

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Acknowledgments

The presented work was performed at the Institute of Astronautics at Technical University of Munich in the frame of the PROSPECT/ProSPA Phase A study in response to AO 7948 of the European Space Agency, as part of the General Studies Programme (GSP). The ProSPA Phase A activity was led by the Open University in Milton Keynes, U.K.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 3May 2017

History

Received: Mar 22, 2016
Accepted: Jul 8, 2016
Published online: Sep 22, 2016
Discussion open until: Feb 22, 2017
Published in print: May 1, 2017

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Authors

Affiliations

Research Assistant, Technical Univ. of Munich, Institute of Astronautics, Boltzmannstrasse 15, 85748 Garching, Germany (corresponding author). E-mail: [email protected]
A. Hoehn
Senior Scientist, Technical Univ. of Munich, Institute of Astronautics, Boltzmannstrasse 15, 85748 Garching, Germany.
U. Walter
Head of Institute, Technical Univ. of Munich, Institute of Astronautics, Boltzmannstrasse 15, 85748 Garching, Germany.
S. Barber
Senior Manager, Dept. of Physical Sciences, Open Univ., Milton Keynes MK7 6AA, U.K.
J. Carpenter
Lead Scientist, European Space Agency, ESTEC, Keplerlaan 1, 2201AZ, Noordwijk, Netherlands.

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