Javascript must be enabled to continue!
ONERA accelerometers for future gravity mission
View through CrossRef
The 2017-2027 Decadal Survey for Earth Science and Applications from Space has identified the Targeted Mass Change Observable as one of 5 Designated Mission. In Europe, ESA has proposed to Ministerial Counsel of November 2019 to begin a Phase A on the Next Generation Gravity Mission.These missions will continue the observation provided by GRACE and GRACE-FO. In these missions and the future concepts, the accelerometer provides either the gravity signal in a gradiometer configuration (GOCE type mission), or the non-gravitational acceleration to be suppressed to the ranging measurement between two satellites (GRACE-type mission).ONERA has procured the accelerometer for all the previous gravity missions (GRACE, GOCE, GRACE-FO) and works to improve the scientific return of the instruments for the future missions.In a frame of a pre-development contract with ESA to increase TRL, Onera is developing its new accelerometer MicroSTAR, a high accuracy accelerometer with 3 sensitive linear acceleration measurements as well as 3 angular acceleration measurements for the attitude control or reconstruction.In parallel, a miniaturized version of MicroSTAR with low accuracy, CubeSTAR accelerometer, is developed with internal funding. CubeSTAR is adapted for constellation or nanosat.An other way is to improve the low-frequency noise of the accelerometer, by hybridization of electrostatic accelerometer with cold atom interferometer.The presentation will detail these developments.
Title: ONERA accelerometers for future gravity mission
Description:
The 2017-2027 Decadal Survey for Earth Science and Applications from Space has identified the Targeted Mass Change Observable as one of 5 Designated Mission.
In Europe, ESA has proposed to Ministerial Counsel of November 2019 to begin a Phase A on the Next Generation Gravity Mission.
These missions will continue the observation provided by GRACE and GRACE-FO.
In these missions and the future concepts, the accelerometer provides either the gravity signal in a gradiometer configuration (GOCE type mission), or the non-gravitational acceleration to be suppressed to the ranging measurement between two satellites (GRACE-type mission).
ONERA has procured the accelerometer for all the previous gravity missions (GRACE, GOCE, GRACE-FO) and works to improve the scientific return of the instruments for the future missions.
In a frame of a pre-development contract with ESA to increase TRL, Onera is developing its new accelerometer MicroSTAR, a high accuracy accelerometer with 3 sensitive linear acceleration measurements as well as 3 angular acceleration measurements for the attitude control or reconstruction.
In parallel, a miniaturized version of MicroSTAR with low accuracy, CubeSTAR accelerometer, is developed with internal funding.
CubeSTAR is adapted for constellation or nanosat.
An other way is to improve the low-frequency noise of the accelerometer, by hybridization of electrostatic accelerometer with cold atom interferometer.
The presentation will detail these developments.
Related Results
Gravity data reduction, Bouguer anomaly, and gravity disturbance
Gravity data reduction, Bouguer anomaly, and gravity disturbance
Each point on the earth has a gravity and gravity potential value. Surfaces formed by connecting points with equal gravity potential values are called equipotential surfaces or lev...
ONERA accelerometers for future gravity mission
ONERA accelerometers for future gravity mission
The 2017-2027 Decadal Survey for Earth Science and Applications from Space has identified the Targeted Mass Change Observable as one of 5 Designated Mission. In Europe, ESA has con...
Using spherical scaling functions in scalar and vector airborne gravimetry
Using spherical scaling functions in scalar and vector airborne gravimetry
<p>Airborne gravimetry is capable to provide Earth&#8217;s gravity data of high accuracy and spatial resolution for any area of interest, in particular for ha...
Concepts for a German Small Sat Mission to (99942) Apophis
Concepts for a German Small Sat Mission to (99942) Apophis
Due to the increased performance of small satellites, their use in the exploration of asteroids is becoming increasingly more important. The DART mission with the CubeSat LICIACube...
Sinking or bouncing in low gravity environments?
Sinking or bouncing in low gravity environments?
Understanding the physics of granular materials in a low gravity and vacuum environment is essential to predict the regolith behavior on the Moon and asteroids. Cohesive forces - i...
The Absolute Gravity Reference Network of Italy
The Absolute Gravity Reference Network of Italy
The project for realizing the reference network for absolute gravity in the Italian area is presented. This fundamental infrastructure is the general frame for all the scientific a...
Improvement of ONERA Electrostatically suspended torsion pendulum
Improvement of ONERA Electrostatically suspended torsion pendulum
In order to meet the objectives of the Next Generation Gravity Mission (NGGM), the French Aerospace Lab ONERA is developing a new accelerometer concept MicroSTAR with three sensiti...
ONERA accelerometers for future gravity mission
ONERA accelerometers for future gravity mission
<p>ONERA (the French Aerospace Lab) is developing, manufacturing and testing ultra-sensitive electrostatic accelerometer for space application. ONERA has procured the...


