Extreme-ultraviolet Stellar Characterization for Atmospheric Physics and Evolution

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Extreme-ultraviolet Stellar Characterization for Atmospheric Physics and Evolution

NASA
Website	escapetelescope.org lasp.colorado.edu/home/cusp/escape/
Mission duration	2 years (design)
Spacecraft properties
Ball Aerospace
Launch mass	245 kg (540 lb)
Dry mass	245 kg (540 lb)
Dimensions	2.57 m × 2.09 m × 1.10 m (8.4 ft × 6.9 ft × 3.6 ft)
Power	256 W
Start of mission
Launch date	2025
Orbital parameters
Reference system	Low Earth Orbit
Main telescope
Type	Gregorian telescope, grazing incidence
Diameter	0.46 m (1.5 ft)
Wavelengths	80 Å to 825 Å (EUV) 1280 Å to 1650 Å (FUV)
ESCAPE mission logo Explorers program ← EUVE

The Extreme-ultraviolet Stellar Characterization for Atmospheric Physics and Evolution (ESCAPE) mission aims to find environments beyond Earth's solar system that might host planets with thick atmospheres to support life.^[1]

The long-term stability of

ESCAPE provides the first comprehensive study of the stellar EUV environments that control atmospheric mass-loss and determine the habitability of rocky exoplanets. ESCAPE's prime mission is driven by two spectroscopic surveys: 1) a broad survey of EUV and FUV flux from 200 nearby (d < 100 pc) F, G, K, and M stars, providing direct input into atmospheric evolution models. The mission targets stars with a range of ages and activity levels, and places an emphasis on stars with known exoplanets. 2) A deep monitoring survey (~2 weeks per star) of 24 targets-of-interest to measure the stellar flare frequency distribution and constrain the coronal mass ejection (CME) rate and high-energy particle fluence from these objects. Together, these surveys provide the crucial stellar drivers that regulate habitable environments on planets targeted by upcoming atmospheric characterization missions, from James Webb Space Telescope to Large Ultraviolet Optical Infrared Surveyor.

The ESCAPE Hettrick-Bowyer telescope comprises a grazing-incidence mirror that focus ultraviolet light through a spectral filter, where a secondary mirror module directs light to a set of grazing-incidence gratings and a set of normal-incidence gratings that disperse light as spectra onto the microchannel plate detector. This ultimately results in spectra ranging from 80 Å to 825 Å (EUV) and from 1280 Å to 1650 Å (FUV) with 1 Å resolution. Once downlinked and processed, these measurements will be accessible on Mikulski Archive for Space Telescopes (MAST).

ESCAPE is being designed and built by several institutions, led by Principal Investigator Kevin France at the Laboratory for Atmospheric and Space Physics (LASP), a research institute at University of Colorado Boulder.

• LASP
  is responsible for the overall project, instrument design, instrument integration, mission operations, and science data processing.
• Ball Aerospace
  provides the spacecraft bus, integrates it with the telescope, and performs spacecraft level environmental testing.
• Marshall Space Flight Center and Smithsonian Astrophysical Observatory jointly manufacture, assembles, and align the concentric, grazing incidence mirrors optimized for ESCAPE's observing bandpass.
• Pennsylvania State University provides the custom gratings that disperse incoming light into spectra.
• University of California Berkeley
  provides the specialized detector.