MISSION DESCRIPTION

 

 

DEMETER (Detection of Electro-Magnetic Emissions Transmitted from Earthquake Regions) is devoted to the investigation of the Earth ionosphere disturbances due to seismic and volcanic activities.

 

 

Scientific Objectives

The scientific objectives of the DEMETER mission are :

-         to study the ionospheric disturbances in relation to the seismic activity and to examine the pre- and post-seismic effects,

-         to study the ionospheric disturbances in relation to the volcano activity,

-         to survey the ionospheric disturbances in relation to the anthropogenic activity,

-         to contribute to the understanding of the generation mechanism of these disturbances,

-         to give a global information on the Earth electromagnetic environment.

 

 

Scientific Payload

To achieve theses goals, DEMETER allows the measurements of the six components of  the electromagnetic wave field in a wide frequency interval and the determination of the plasma parameters, ion composition, electron density and temperature, energetic electron flux.

 

The science payload is composed of  five instruments :

-         ICE, three electric sensors from DC up to 3.5 MHz,

-         IMSC, three magnetic sensors from a few Hz up to 18 kHz,

-         IAP, an ion analyzer,

-         IDP, an energetic particle detector,

-         ISL, a Langmuir probe,

associated with the BANT common electronic module for onboard data processing and handling.

 

A large onboard memory (8Gbits) is used to collect the data all around the Earth and a high bit rate telemetry in X band (16 Mb/s) will download these data.

 

 

Working Modes

DEMETER has two science modes of operation:

(i)                  the Survey mode collecting averaged data all around the Earth; onboard processing are performed to reduce the telemetry flow to 25 kb/s;

(ii)                the Burst mode collecting data with a high bit rate of 1.7 Mb/s above the seismic regions.

 

The triggering of the Burst mode is automatically realized when the satellite crosses a seismic zone defined in the programmation plan.

 

 

Orbit parameters

DEMETER is a micro-satellite (130 kg) with a low-altitude of 710 km and an inclination of 98.3°.

 

 

Mission Phases

Demeter has been successfully launched on June 29 at 6h30 UT by a Dnepr rocket from Baļkonour.