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Department of Physics
Credit: Jack Hobhouse

Dr Tristram Warren

Head of Infrared Multilayer Laboratory

Sub department

  • Professional and support services

Research groups

  • Planetary surfaces
  • Solar system
  • Space instrumentation
Tristram.Warren@physics.ox.ac.uk
Telephone: 01865 (2)82436
Atmospheric Physics Clarendon Laboratory, room 304
  • About
  • Publications

Full-Band Signal Extraction From Sensors in Extreme Environments: The NASA InSight Microseismometer

IEEE Sensors Journal Institute of Electrical and Electronics Engineers (IEEE) 18:22 (2018) 9382-9392

Authors:

Alexander E Stott, Constantinos Charalambous, Tristram J Warren, William T Pike
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The Oxford space environment goniometer: A new experimental setup for making directional emissivity measurements under a simulated space environment

Review of Scientific Instruments American Institute of Physics 88:12 (2017) 124502

Authors:

Tristram J Warren, Neil E Bowles, Kerri Donaldson Hanna, IR Thomas

Abstract:

Measurements of the light scattering behaviour of the regoliths of airless bodies via remote sensing techniques in the Solar System, across wavelengths from the visible to the far infrared, are essential in understanding their surface properties. A key parameter is knowledge of the angular behaviour of scattered light, usually represented mathematically by a phase function. The phase function is believed to be dependent on many factors including the following: surface composition, surface roughness across all length scales, and the wavelength of radiation. Although there have been many phase function measurements of regolith analog materials across visible wavelengths, there have been no equivalent measurements made in the thermal infrared (TIR). This may have been due to a lack of TIR instruments as part of planetary remote sensing payloads. However, since the launch of Diviner to the Moon in 2009, OSIRIS-Rex to the asteroid Bennu in 2016, and the planned launch of BepiColombo to Mercury in 2018, there is now a large quantity of TIR remote sensing data that need to be interpreted. It is therefore important to extend laboratory phase function measurements to the TIR. This paper describes the design, build, calibration, and initial measurements from a new laboratory instrument that is able to make phase function measurements of analog planetary regoliths across wavelengths from the visible to the TIR.
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CASTAway: An asteroid main belt tour and survey.

Advances in Space Research Elsevier 62:8 (2017) 1998-2025

Authors:

Neil E Bowles, C Snodgrass, JP Sanchez, Jessica A Arnold, P Eccleston, T Andert, A Probst, G Naletto, AC Vandaele, de de Leon, A Nathues, IR Thomas, N Thomas, L Jorda, V da Deppo, H Haack, SF Green, B Carry, Kerri L Donaldson Hanna, J Leif Jorgensen, A Kereszturi, FE DeMeo, JK Davies, Fraser Clarke, K Kinch, A Guilbert-Lepoutre, J Agarwal, AS Rivkin, P Pravec, S Fornasier, M Gravnik, RH Jones, N Murdoch, KH Joy, Matthias Tecza, Jennifer M Barnes, J Licandro, BT Greenhagen, Simon B Calcutt, Charlotte M Marriner, Tristram J Warren, I Tosh

Abstract:

CASTAway is a mission concept to explore our Solar System’s main asteroid belt. Asteroids and comets provide a window into the formation and evolution of our Solar System and the composition of these objects can be inferred from space-based remote sensing using spectroscopic techniques. Variations in composition across the asteroid populations provide a tracer for the dynamical evolution of the Solar System. The mission combines a long-range (point source) telescopic survey of over 10,000 objects, targeted close encounters with 10 – 20 asteroids and serendipitous searches to constrain the distribution of smaller (e.g. 10 m) size objects into a single concept. With a carefully targeted trajectory that loops through the asteroid belt, CASTAway would provide a comprehensive survey of the main belt at multiple scales. The scientific payload comprises a 50 cm diameter telescope that includes an integrated low-resolution (R = 30 – 100) spectrometer and visible context imager, a thermal (e.g. 6 – 16 μm) imager for use during the flybys, and modified star tracker cameras to detect small (~10 m) asteroids. The CASTAway spacecraft and payload have high levels of technology readiness and are designed to fit within the programmatic and cost caps for a European Space Agency medium class mission, whilst delivering a significant increase in knowledge of our Solar System.
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