Payload System Design, Integration, and Verification Challenges for an Academically Centered Flight Instrument Development

The single-instrument payload for the SPHEREx (Spectro-Photometer for the History of the Universe, Epoch of Reionization, and Ices Explorer) mission was designed, integrated, and tested by an institutionally and culturally diverse team forged from academic, industry, and NASA lab environments. In this paper we describe the challenges encountered and solutions adopted through the implementation of the SPHEREx payload. In particular, we describe the approach that guided the design phase and how, during the integration, testing, and verification phases, and under the pressures of a global pandemic, the strengths of each team were leveraged.

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Published
2025-03-01
DOI
https://doi.org/10.1109/aero63441.2025.11068194
Primary Topic
Spacecraft Design and Technology
Type
article
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article

Payload System Design, Integration, and Verification Challenges for an Academically Centered Flight Instrument Development

Thomas Meredith Brown, Konstantin Penanen, Thomas P. Disarro, Amelia Quon et al.
Spacecraft Design and Technology
article

Payload System Design, Integration, and Verification Challenges for an Academically Centered Flight Instrument Development

Thomas Meredith Brown, Konstantin Penanen, Thomas P. Disarro, Amelia Quon, Paul D. MacNeal, Phil Korngut, Sara Susca, James Wincentsen, Giacomo Mariani, H. Hui, R. Williamson, Bradley Moore, Chi H. Nguyen, S. Padin, Jennifer Rocca
article en

Abstract

The single-instrument payload for the SPHEREx (Spectro-Photometer for the History of the Universe, Epoch of Reionization, and Ices Explorer) mission was designed, integrated, and tested by an institutionally and culturally diverse team forged from academic, industry, and NASA lab environments. In this paper we describe the challenges encountered and solutions adopted through the implementation of the SPHEREx payload. In particular, we describe the approach that guided the design phase and how, during the integration, testing, and verification phases, and under the pressures of a global pandemic, the strengths of each team were leveraged.

California Institute of Technology (US), Jet Propulsion Laboratory (US)
Openalex Percentile: Top 77%
Spacecraft Design and Technology
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Payload System Design, Integration, and Verification Challenges for an Academically Centered Flight Instrument Development — Thomas Meredith Brown, Konstantin Penanen, et al. · (2025) | TGRS Research Map | TGRS