TY - GEN
T1 - GRATTIS
T2 - 2024 Small Satellites Systems and Services Symposium, 4S 2024
AU - Conklin, John W.
AU - Apple, Stephen
AU - Álvarez, Anthony Dávila
AU - Bennett, Stephen
AU - Bevilacqua, Riccardo
AU - Bischof, Lea
AU - Conroy, Joseph
AU - Footdale, Joseph
AU - Forrester, Zane
AU - Fulda, Paul
AU - Hanson, John
AU - Hollis, Harold
AU - Kennedy, Victoria
AU - Kinzie, Ryan
AU - Perkins, Cole
AU - Sanjuan, Jose
AU - Schwarze, Thomas
AU - Siu, John
AU - Spero, Robert
AU - Storm, Mark
AU - Ware, Brent
AU - Wass, Peter
AU - Wiese, David
N1 - Publisher Copyright: © 2025 The Authors.
PY - 2025
Y1 - 2025
N2 - The Gravitational Reference Advanced Technology Test In Space (GRATTIS) mission will demonstrate the end-to-end functionality and sensitivity performance of the Simplified Gravitational Reference Sensor (S-GRS), an ultra-precise inertial sensor for future Earth geodesy missions. These sensors are used to measure or compensate for all non-gravitational accelerations of the host spacecraft so that they can be removed in the data analysis to recover spacecraft motion due to Earth’s gravity field, the main science observable. The S-GRS concept is a simplified version of the flight-proven LISA Pathfinder GRS. It consists of a free-falling cubic test mass inside an electrode housing that senses the position and orientation of the test mass and electrostatically applies forces and torques to it to keep it centered at a nanometer-level. The improved performance of the S-GRS is enabled by removing the small grounding wire used in the GRACE accelerometers, which limits its performance, and replacing it with a UV LED-based charge management system, increasing the mass of the sensor’s TM, and increasing the gap between the TM and its electrode housing. GRATTIS will fly two identical S-GRS mounted next to one another at the center of mass of a 160 kg ESPA-class commercial microsatellite with a planned launch in 2027. The six-axis acceleration measurement capability of the S-GRS allows precision measurement of the spacecraft drag-induced translational acceleration, as well as the residual angular acceleration of the nominally inertially-pointed bus. By combining the outputs of each sensor and with the known relative position of the two TMs, we can recover the acceleration sensitivity (noise floor) of the S-GRS.
AB - The Gravitational Reference Advanced Technology Test In Space (GRATTIS) mission will demonstrate the end-to-end functionality and sensitivity performance of the Simplified Gravitational Reference Sensor (S-GRS), an ultra-precise inertial sensor for future Earth geodesy missions. These sensors are used to measure or compensate for all non-gravitational accelerations of the host spacecraft so that they can be removed in the data analysis to recover spacecraft motion due to Earth’s gravity field, the main science observable. The S-GRS concept is a simplified version of the flight-proven LISA Pathfinder GRS. It consists of a free-falling cubic test mass inside an electrode housing that senses the position and orientation of the test mass and electrostatically applies forces and torques to it to keep it centered at a nanometer-level. The improved performance of the S-GRS is enabled by removing the small grounding wire used in the GRACE accelerometers, which limits its performance, and replacing it with a UV LED-based charge management system, increasing the mass of the sensor’s TM, and increasing the gap between the TM and its electrode housing. GRATTIS will fly two identical S-GRS mounted next to one another at the center of mass of a 160 kg ESPA-class commercial microsatellite with a planned launch in 2027. The six-axis acceleration measurement capability of the S-GRS allows precision measurement of the spacecraft drag-induced translational acceleration, as well as the residual angular acceleration of the nominally inertially-pointed bus. By combining the outputs of each sensor and with the known relative position of the two TMs, we can recover the acceleration sensitivity (noise floor) of the S-GRS.
UR - https://www.scopus.com/pages/publications/105002250927
UR - https://www.scopus.com/pages/publications/105002250927#tab=citedBy
U2 - 10.1117/12.3061925
DO - 10.1117/12.3061925
M3 - Conference contribution
T3 - Proceedings of SPIE - The International Society for Optical Engineering
BT - Small Satellites Systems and Services Symposium, 4S 2024
A2 - de Mallorca, Palma
PB - SPIE
Y2 - 27 May 2024 through 31 May 2024
ER -