DocumentCode :
711281
Title :
Design and demonstration of the Mars Organic Molecule Analyzer (MOMA) on the ExoMars 2018 rover
Author :
Arevalo, Ricardo ; Brinckerhoff, William ; van Amerom, Friso ; Danell, Ryan ; Pinnick, Veronica ; Xiang Li ; Getty, Stephanie ; Hovmand, Lars ; Grubisic, Andrej ; Mahaffy, Paul ; Goesmann, Fred ; Steininger, Harald
Author_Institution :
NASA Goddard Space Flight Center (GSFC), Greenbelt, MD, USA
fYear :
2015
fDate :
7-14 March 2015
Firstpage :
1
Lastpage :
11
Abstract :
The Mars Organic Molecule Analyzer (MOMA) investigation is a key astrobiology experiment scheduled to launch on the joint ESA-Roscosmos ExoMars 2018 rover mission. MOMA will examine the chemical composition of geological samples acquired from depths of up to two meters below the martian surface, where fragile organic molecules may be protected from destructive cosmic radiation and/or oxidative chemical reactions. The heart of the MOMA mass spectrometer subsystem (i.e., MOMA-MS) is a miniaturized linear ion trap (LIT) that supports two distinct modes of operation to detect: i) volatile and semi-volatile, low-to-moderate mass organics (≤500 Da) via pyrolysis coupled with gas chromatography mass spectrometry (pyr/GCMS); and, ii) more refractory, moderate-to-high mass compounds (up to 1000 Da) via laser desorption (LDMS) at ambient Mars pressures. Additionally, the LIT mass analyzer enables selective ion trapping via multi-frequency waveform ion excitation (e.g., stored waveform inverse Fourier transform, or SWIFT), and structural characterization of complex molecules using tandem mass spectrometry (MS/MS). A high-fidelity Engineering Test Unit (ETU) of MOMA-MS, including the LIT subassembly, dual-gun electron ionization source, micropirani pressure gauge, solenoid-driven aperture valve, redundant detection chains, and control electronics, has been built and tested at NASA GSFC under relevant operational conditions (pressure, temperature, etc.). Spaceflight qualifications of individual hardware components and integrated subassemblies have been validated through vibration, shock, thermal, lifetime, and performance evaluations. The ETU serves as a pathfinder for the flight model buildup, integration and test, as the ETU meets the form, fit and function of the flight unit that will be delivered to MPS in late 2015. To date, the ETU of MOMA-MS has been shown to meet or exceed all functional requirements, including mass range, resolution, accuracy, instrumental drif- , and limit-of-detection specifications, thereby enabling the primary science objectives of the MOMA investigation and ExoMars 2018 mission.
Keywords :
Fourier transforms; Mars; chromatography; cosmic background radiation; planetary rovers; ExoMars 2018 Rover; Fourier transform; MOMA mass spectrometer subsystem; Mars Organic Molecule Analyzer; Mars pressures; astrobiology experiment; chemical composition; cosmic radiation; fragile organic molecules; gas chromatography mass spectrometry; geological samples; laser desorption; low-to-moderate mass organics; miniaturized linear ion trap; multi-frequency waveform; oxidative chemical reactions; pyrolysis; tandem mass spectrometry; Apertures; Biographies; Chemical lasers; Ovens; Payloads; Spectroscopy; Valves;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2015 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5379-0
Type :
conf
DOI :
10.1109/AERO.2015.7119073
Filename :
7119073
Link To Document :
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