The slitless spectrometer plays an important role in the WFIRST mission for the survey of emission-line galaxies. This will be an unprecedented very wide field, HST quality 3D survey of emission line galaxies 1 . The concept of the compound grism as a slitless spectrometer has been presented previously. The presentation briefly discusses the challenges and solutions of the optical design, and recent specification updates, as well as a brief comparison between the prototype and the latest design. However, the emphasis of this paper is the progress of the grism prototype: the fabrication and test of the complicated diffractive optical elements and powered prism, as well as grism assembly alignment and testing. Especially how to use different tools and methods, such as IR phase shift and wavelength shift interferometry, to complete the element and assembly tests. The paper also presents very encouraging results from recent element tests to assembly tests. Finally we briefly touch the path forward plan to test the spectral characteristic, such as spectral resolution and response.

Hyperspectral snapshot imagers are capable of producing 2D spatial images with a single exposure at selected and numerous wavelength bands instead of 1D spatial at all spectral band images like in push-broom instruments. Snapshot imagers are critical technologies for multi-angle remote sensing using distributed space missions. They help to relax the attitude control requirements of clusters of small satellites whose narrow field-of-view payloads point at the same ground spot or to increase the footprint area of small satellite constellations with wide field-of-view payloads. This paper reviews the existing spectral imagers for multi-angle remote sensing, performs a feasibility study to incorporate existing state-of-the-art snapshot imagers and proposes baseline imagers to serve as payload for the distributed nanosatellites. The overall approach includes an extensive trade study to identify the optics, spectral elements, their parameters and compare the identified choices both qualitatively and quantitatively. The proposed baseline design has an telescope aperture diameter of 7 cm, focal plane pixel size of 20 μm, 1000 pixels per side of the focal plane array sampling the scene and acousto-optic tunable filters or waveguide spatial heterodyne imagers that simulate a swath up to 90 km, image up to 86 wavebands with an SNR above 100. The tradeoff between spectral and spatial ranges sampled by the two baseline imager options has been highlighted.

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