Official name MMS 1
Alternative name MMS 1
Cospar ID 2015-011A
Norad ID 40482
Launch date 2015-03-13
Launch site AFETR
Launch vehicle Atlas-5(421)¹
Country/Organization USA
Type application Magnetospheric Research
Operator NASA SwRI
RCS size LARGE
Decay date ON ORBIT
Period (min) 5055.4
Inclination (deg) 45.65
Perigee (km) 2271
Apogee (km) 180119
Eccentricity 0.975097318931959
Mean motion (revs. per day) 0.284843929263758
Semi-Major axis (km) 97573.135
Raan (deg) 14.2306
Arg of perigee (deg) 144.1654
Shape Cyl + 1 Ant
Mass (kg) 1360
Diameter (m) 3.6
Height (m) 1.2
Span (m^2) 112
Lifetime 2.5 years
Contractors NASA SwRI
Equipment see above
Power Solar cells, batteries

MMS (Magnetospheric Multiscale) is a Solar-Terrestrial Probe mission comprising four identically instrumented spacecraft to discover the fundamental physics of magnetic reconnection using Earth's magnetosphere as a laboratory.

The four identically instrumented spin-stabilized spacecraft were launched on a single expendable launch vehicle and configured in a tetrahedral formation to probe dayside and nightside reconnection regions.

The MMS spacecraft are being developed at NASA's Goddard Space Flight Center (GSFC) in Greenbelt, Maryland. GSFC is also responsible for the overall management of the MMS mission and mission operations. The mission is to be launched in October 2014 and will have an duration of two years (Prime Mission) + 6 months (launch, checkout, commissioning)

Orbit: 1.2 Earth radii by 12 Earth radii (day side); 1.2 Earth radii by 25 Earth radii (night side)

The four MMS spacecraft will carry identical suites of plasma analyzers, energetic particle detectors, magnetometers, and electric field instruments as well as a device to prevent spacecraft charging from interfering with the highly sensitive measurements required in and around the diffusion regions. The plasma and fields instruments will measure the ion and electron distributions and the electric and magnetic fields with unprecedentedly high (millisecond) time resolution and accuracy. These measurements will enable to MMS to locate and identify the small (1-10 km) and rapidly moving (10-100 km/s) diffusion regions, to determine their size and structure, and to discover the mechanism(s) by which the frozen-in condition is broken, the ions and electrons become demagnetized, and the magnetic field is re-configured. MMS will make the first unambiguous measurements of plasma composition at reconnection sites, while energetic particle detectors will remotely sense the regions where reconnection occurs and determine how reconnection processes produce such large numbers of energetic particles.

Instrument Suite on the satellites will consist of:

  • Fast Plasma Instrument;
  • FIELDS;
  • Hot Plasma Composition Analyzer;
  • Energetic Particles;
  • Active Spacecraft Potential Control;
  • Central Instrument Data Processor
Satellite COSPAR Date LS Launch Vehicle Remarks
MMS 1 2015-011A 2015-03-13 AFETR Atlas-5(421)¹ with MMS 2, 3, 4
MMS 2 2015-011B 2015-03-13 AFETR Atlas-5(421)¹ with MMS 1, 3, 4
MMS 3 2015-011C 2015-03-13 AFETR Atlas-5(421)¹ with MMS 1, 2, 4
MMS 4 2015-011D 2015-03-13 AFETR Atlas-5(421)¹ with MMS 1, 2, 3