The Lunar Trailblazer Lunar Thermal Mapper Instrument

Journal of Geophysical Research Planets American Geophysical Union (AGU) 131:5 (2026)

Authors:

Neil E Bowles, Bethany L Ehlmann, Rory Evans, Tristram J Warren, Henry H Eshbaugh, Greg King, Waqas Mir, Namrah Habib, Katherine Shirley, Fraser Clarke, Cyril Bourgenot, Chris Howe, Keith Nowicki, Fiona HM Henderson, Christopher S Edwards, Rachel L Klima, Kerri Donaldson Hanna, Calina C Seybold, Andrew T Klesh, David R Thompson, Elise Furlan, Elena Scire, Judy S Adler, Nicholas Elkington, Aria Vitkova, Jon Temple, Simon Woodward

Abstract:

Abstract The Lunar Thermal Mapper (LTM) instrument is a UK Space Agency funded infrared radiometer designed and built for the National Aeronautics and Space Administration Lunar Trailblazer mission launched in February 2025. LTM is a pushbroom imaging filter radiometer with 15 channels that cover the wavelength range from 6.25 to 100 μm with a 40–70 m/pixel ground sampling. Lunar Trailblazer's mission is to understand the form, abundance and distribution of water across the lunar surface. LTM provides an independent measure of temperature to investigate thermal effects on water's mapped distribution as well as an independent measure of surface mineralogy. The LTM instrument's 15 infrared channels include four broadband temperature sensing channels (6.25–12.5, 12.5–25, 25–50 and 50–100 μm) plus 11 additional narrow band (∼40 cm −1 ) filters from ∼7–10 μm to map and discriminate silicate composition. We review the LTM design and calibration campaign at the University of Oxford's Space Instrumentation facility and show that the instrument has sensitivity from 400 K with a Noise Equivalent Temperature Difference of <0.1 K to <1 K at 110 K for typical integration times (e.g., 30 Hz readout) from a nominal 70–130 km lunar orbit design altitude. Plain Language Summary This paper describes the Lunar Thermal Mapper instrument for NASA's Lunar Trailblazer mission. Lunar Thermal Mapper is a thermal imaging system designed to sense the temperature and composition of the lunar surface using the thermal infrared. By sensing the temperature environment of the Moon, Lunar Thermal Mapper supports the Trailblazer's mission to map water on the lunar surface. Key Points The Lunar Thermal Mapper (LTM) instrument will measure thermal infrared radiation from the Moon across from 400 K to <110 K The LTM instrument completed assembly, testing, calibration and integration on the Lunar Trailblazer spacecraft The LTM instrument demonstrated sensitives of <0.1 K at 400 K and <1 K at 110 K during ground testing and calibration

New vision of the Saturnian system in the context of a highly dissipative Saturn – editorial

Space Science Reviews Springer Nature 222:4 (2026) 38

Authors:

Valéry Lainey, Michel Blanc, Aurélien Crida, Jeffrey N Cuzzi, Maryame El Moutamid, Gianrico Filacchione, Carly Howett, Alyssa Rhoden, Tilman Spohn

Thermophysical Properties of Europa's Surface Constrained by Galileo Photopolarimeter-Radiometer Temperature Measurements

(2026)

Authors:

L Lange, S Piqueux, PO Hayne, C Mergny, A Le Gall, F Schmidt, J Rathbun, J Spencer, K Sorli, S Howes, C Howett, CS Edwards, PR Christensen

Morphometric Properties of the CP-21 Landing Site on the Moon at Mons Gruithuisen Gamma

The Planetary Science Journal IOP Publishing 7:4 (2026) 78

Authors:

Jean-Pierre Williams, Sarah Valencia, Kristen A Bennett, Margaret E Landis, Kerri L Donaldson Hanna, Adrienne Dove, Patrick O’Brien, Brett W Denevi, Justin Hagerty, Craig Hardgrove, Paul O Hayne, Adam LaMee, Thomas H Prettyman, Katherine A Shirley, Matthew A Siegler, Jessica M Sunshine

Abstract:

Characterizing terrain surface properties is an essential step in assessing the feasibility of landing successfully at a location on a planetary surface. Slopes and terrain ruggedness index (TRI) values derived from high-resolution (2 m pixel−1) digital terrain models provided important constraints in selecting the landing site for the upcoming Payloads and Research Investigations on the Surface of the Moon program as part of the Commercial Lunar Payload Services task order CP-21 mission. The selected landing site needed to balance safety requirements with the ability to achieve the science and exploration goals of the Lunar Vulkan Imaging and Spectroscopy Explorer payload. In this study, we compare several morphometric parameters in the context of the CP-21 landing site on Mons Gruithuisen Gamma, or the Gamma dome, and quantify the information they convey about lunar surface properties to assess their utility for future landing site evaluation. TRI was found to be a useful metric for assessing landing site safety. Metrics that better decouple slope and surface roughness, the vector ruggedness measure and the standard deviation of slope, provided additional information about surface characteristics and textures such as the degree to which roughness is isotropic.

Spectral Similarity in the Thermal Infrared between Sulfide-rich Carbonaceous Chondrite Meteorites, Jupiter Trojans, and Other D- and P-type Asteroids

The Planetary Science Journal American Astronomical Society 7:4 (2026) 90

Authors:

Helena C Bates, Ashley J King, Kerri L Donaldson Hanna, Audrey C Martin, Joshua P Emery, Neil E Bowles, Sara S Russell

Abstract:

Carbonaceous chondrite meteorites, which include the sulfide-rich “Yamato-type” chondrites (CYs), have undergone a complex history of aqueous and thermal alteration and offer crucial insights into early outer solar system conditions. In this study, we evaluate thermal infrared (TIR) reflectance spectra of three CY chondrites. We observe a broad spectral plateau near 10 μm, a spectral signature that has been observed in remote observations of some primitive, low-albedo asteroids, including Jupiter Trojans. We compare our data to CY emissivity spectra, spectra of Fe-sulfide and olivine mixtures, and remote Jupiter Trojan observations and establish the plateau and low albedo are a result of a high content of fine-particulate Fe-sulfide of these meteorites. We therefore suggest that D- and P-type asteroids, like Jupiter’s Trojan asteroids, could have a high abundance of Fe sulfide on their surfaces as a potential result of aqueous alteration followed by dehydration, shedding light on the processes shaping the outer solar system.