Official name RBSP A
Alternative name Radiation Belt Storm Probe 1
Cospar ID 2012-046A
Norad ID 38752
Launch date 2012-08-30
Launch site AFETR
Launch vehicle Atlas-5(401)
Country/Organization USA
Type application Magnetospheric Research
Operator NASA JHU/APL
RCS size LARGE
Decay date ON ORBIT
Period (min) 410.12
Inclination (deg) 9.7
Perigee (km) 203
Apogee (km) 23611
Eccentricity 0.982951205173427
Mean motion (revs. per day) 3.51116746318151
Semi-Major axis (km) 18285.135
Raan (deg) 261.1549
Arg of perigee (deg) 291.063
Shape Oct Cyl + 4 Pan + 8 Rod
Mass (kg) 591.6
Diameter (m) 1.8
Height (m) 1.3
Span (m^2) 101.7
Lifetime 2 years (design); 7 years (achieved)
Contractors NASA JHU/APL
Equipment EXT, EMFISIS, EFW, RBSPICE, RPS
Propulsion 8 × MR-103G monopropellant thrusters
Configuration Octagonal prism, spin stabilzed
Power 4 deployable fixed solar arrays, batteries

The RBSP (Radiation Belt Storm Probes) Mission, part of NASA's Living With a Star program, will provide unprecedented insight into the physical dynamics of the radiation belts and give scientists the data they need to make predictions of changes in this critical region of space.

After launch in 2012, two spacecraft will orbit the Earth, sampling the harsh radiation belt environment where major space weather activity occurs and many spacecraft operate. The mission was originally baselined for a Delta-7925 launch from Cape Canaveral, but an Atlas-5(401) launch vehicle was selected.

The two spacecraft will measure the particles, magnetic and electric fields, and waves that fill geospace. Only with two spacecraft taking identical measurements and following the same path, can scientists begin to understand how the belts change in both space and time.

The RBSP spacecraft will carry a number of instruments and instrument suites to support five experiments that will address the mission's science objectives. Because it is vital that the two craft make identical measurements to observe changes in the radiation belts through both space and time, each probe will carry the following instruments:

  • Energetic Particle, Composition, and Thermal Plasma Suite (ECT)
  • Electric and Magnetic Field Instrument Suite and Integrated Science (EMFISIS)
  • Electric Field and Waves Suite (EFW)
  • Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE)
  • Relativistic Proton Spectrometer (RPS)

The RBSP propulsion subsystem is a monopropellant hydrazine system that provides orbit maintenance, spin-rate adjustments, and changes in velocity for each spacecraft. The propulsion system consists of eight 0.9 Newton Aerojet MR-103G thrusters. The propellant and pressurant are stored in the three identical tanks, which are spaced equally around the spacecraft spin axes.

In November 2012 the two RBSP probes were renamed Van Allen Probes.

One of the probes was shut down in late July 2019, the second was shut down in September 2019.

Satellite COSPAR Date LS Launch Vehicle Remarks
RBSP A 2012-046A 2012-08-30 AFETR Atlas-5(401) with RBSP B
RBSP B 2012-046B 2012-08-30 AFETR Atlas-5(401) with RBSP A