Official name MICROSCOPE
Alternative name Microscope
Cospar ID 2016-025B
Norad ID 41457
Launch date 2016-04-25
Launch site FRGUI
Launch vehicle Soyuz-ST-A Fregat-M
Country/Organization France
Type application Science
Operator CNES
RCS size LARGE
Decay date ON ORBIT
Period (min) 98.87
Inclination (deg) 98.26
Perigee (km) 703
Apogee (km) 706
Eccentricity 0.0021291696238467
Mean motion (revs. per day) 14.5645797511884
Semi-Major axis (km) 7082.635
Raan (deg) 133.072
Arg of perigee (deg) 85.8486
Shape Box + 2 Pan
Mass (kg) 303
Height (m) 1.3
Width (m) 0.9
Depth (m) 1.3
Span (m^2) 1.3
Lifetime 2 years
Contractors CNES
Equipment T-SAGE
Propulsion cold-gas microthrusters
Configuration Myriade
Power Solar cells, batteries

The MICROSCOPE (Microsatellite à traînée Compensée pour l'Observation du Principe d'Equivalence) mission has been selected at end of 1999 by the French space agency Cnes for a launch scheduled for late 2004. The MICROSCOPE satellite developed by CNES within its Myriade line of product, weights 300 kg and is compatible with a low cost launch like ASAP Ariane-5.

The scientific objective of the mission is the test of the Equivalence Principle (EP) up to an accuracy of 10-15 with its well known manifestation, the universality of free fall. This principle, at the origin of general relativity, is only consolidated by experimental results and presently with an accuracy of several 10-13.

To achieve this, two concentric cylindrical test masses made of different materials?one titanium and one a platinum-rhodium alloy?will be minutely controlled to maintain them motionless with respect to the satellite inside independent differential electrostatic accelerometers. If the equivalence principle is verified, the two masses will be subjected to the same control acceleration. If different accelerations have to be applied, the principle will be violated: an event that would shake the foundations of physics.

The experiment is flown on a 303 kg microsatellite – heavier than a usual 100-150 kg microsatellite – built around CNES?s Myriade bus and equipped with cold-gas microthrusters capable of compensating for the tiniest trajectory perturbations that might otherwise skew its results.

Some involved technologies shall prepare the participation of european team to the future more ambious EP experiment in space: STEP mission.

Satellite COSPAR Date LS Launch Vehicle Remarks
MICROSCOPE 2016-025B 2016-04-25 FRGUI Soyuz-ST-A Fregat-M with Sentinel 1B, AAUSAT 4, e-st@r 2, OUFTI 1