CASPA-ADM: a mission concept for observing thermospheric mass density

Author:

Siemes ChristianORCID,Maddox Stephen,Carraz Olivier,Cross Trevor,George Steven,van den IJssel Jose,Kiss-Toth Marton,Pastena Massimiliano,Riou Isabelle,Salter Mike,Sweeney Helen,Trigatzis Mike,Valenzuela Tristan,Visser Pieter

Abstract

AbstractCold Atom technology has undergone rapid development in recent years and has been demonstrated in space in the form of cold atom scientific experiments and technology demonstrators, but has so far not been used as the fundamental sensor technology in a science mission. The European Space Agency therefore funded a 7-month project to define the CASPA-ADM mission concept, which serves to demonstrate cold-atom interferometer (CAI) accelerometer technology in space. To make the mission concept useful beyond the technology demonstration, it aims at providing observations of thermosphere mass density in the altitude region of 300–400 km, which is presently not well covered with observations by other missions. The goal for the accuracy of the thermosphere density observations is 1% of the signal, which will enable the study of gas–surface interactions as well as the observation of atmospheric waves. To reach this accuracy, the CAI accelerometer is complemented with a neutral mass spectrometer, ram wind sensor, and a star sensor. The neutral mass spectrometer data is considered valuable on its own since the last measurements of atmospheric composition and temperature in the targeted altitude range date back to 1980s. A multi-frequency GNSS receiver provides not only precise positions, but also thermosphere density observations with a lower resolution along the orbit, which can be used to validate the CAI accelerometer measurements. In this paper, we provide an overview of the mission concept and its objectives, the orbit selection, and derive first requirements for the scientific payload.

Funder

european space agency

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Compact cold atom accelerometer payload for low-Earth orbit atmospheric drag measurement;2022 IEEE International Symposium on Inertial Sensors and Systems (INERTIAL);2022-05-08

2. Embedded cold atom accelerometer for atmospheric drag measurement;PROC SPIE;2022

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