Sheridan, S.; Barber, S. J.; Morgan, G. H.; Morse, A. D. and Wright, I. P.
|Google Scholar:||Look up in Google Scholar|
Mass spectrometry is one of the most powerful and widely applicable analytical techniques available to planetary scientists, and mass spectrometers of various types have traditionally formed the heart of many spacecraft orbiter, probe and lander payloads. However, they have also been relatively resource intensive, placing substantial mass and power constraints on mission architectures, putting mass spectrometry beyond the reach of some smaller mission payloads. Recent advances in ionisation, analyser and detection components allow smaller instruments to be built bringing mass spectrometry into the reach of smaller spacecraft platforms. Taking two recent examples, the 4.5 kg GC/MS Ptolemy on the Rosetta lander Philae, and the 6.5 kg Gas Analysis Package on Beagle2 as a starting point we will outline the status of a new generation of future instrumentation, including a 2 kg dust composition detector for a Europa orbiter mission proposal, a 500 g device to analyse volatiles in permanently shaded Lunar regions, a 150 g instrument designed to be carried on a mole or melting probe, and a sub-100 gram mass spectrometer for use in planetary microprobes.
|Item Type:||Conference Item|
|Copyright Holders:||2007 The Authors|
|Academic Unit/Department:||Faculty of Science, Technology, Engineering and Mathematics (STEM) > Physical Sciences
Faculty of Science, Technology, Engineering and Mathematics (STEM)
|Interdisciplinary Research Centre:||Centre for Earth, Planetary, Space and Astronomical Research (CEPSAR)|
|Depositing User:||Simon Sheridan|
|Date Deposited:||13 Jun 2012 12:33|
|Last Modified:||02 Aug 2016 14:18|
|Share this page:|