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EQUULEUS

EQUULEUS [JAXA]

EQUULEUS (Equilibrium Lunar-Earth point 6U Spacecraft) is a small lunar mission designed jointly by the Japan Aerospace Exploration Agency (JAXA) and the University of Tokyo.

It will measure the distribution of plasma that surrounds the Earth to help scientists understand the radiation environment in the region of space around Earth. It will also demonstrate low-energy trajectory control techniques, such as multiple lunar flybys, within the Earth-Moon Lagrangian points (EML).

EQUULEUS is equipped with the AQUARIUS propulsion system consisting of eight water thrusters also used for attitude control and momentum management. The spacecraft will carry 1.5 kg of water, and the complete propulsion system occupies about 2.5 units out of the 6 units total spacecraft volume.

The scientific payload consists of three instruments:

  • PHOENIX (Plasmaspheric Helium ion Observation by Enhanced New Imager in eXtreme ultraviolet), a small UV telescope to operate in the high-energy extreme ultraviolet wavelengths. It consists of an entrance mirror of 60 mm diamemeter, and a photon counting device.
  • DELPHINUS (DEtection camera for Lunar impact PHenomena IN 6U Spacecraft), a camera connected to the PHOENIX telescope to observe lunar impact flashes and near-Earth asteroids, as well as potential 'mini-moons' while positioned at the Earth-Moon Lagrangian point L2 (EML2) halo orbit.
  • CLOTH (Cis-Lunar Object Detector within Thermal Insulation) to detect and evaluate the meteoroid impact flux in the cislunar space by using dust detectors mounted on the exterior of the spacecraft.

EQUULEUS is one of 13 cubesats planned to be carried with the Orion EM1 mission into a heliocentric orbit in cis-lunar space on the maiden flight of the SLS (Block 1) iCPS launch vehicle in 2019.

Nation: Japan
Type / Application: Lunar flyby
Operator: JAXA, University of Tokyo
Contractors: JAXA, University of Tokyo
Equipment: PHOENIX, DELPHINUS, CLOTH
Configuration: CubeSat (6U)
Propulsion: AQUARIUS with 8 water thrusters
Power: 2 deployable solar arrays, batteries
Lifetime:
Mass: ~14 kg
Orbit: Lunar fly-by, Earth-Moon Lagrangian points
Satellite COSPAR Date LS Launch Vehicle Remarks
EQUULEUS - 2020 CCK LC-39B SLS (Block 1) iCPS with Orion EM1, BioSentinel, CuSP, LunaH-Map, Lunar-Flashlight, Lunar-IceCube, NEA-Scout, SkyFire, OMOTENASHI, ArgoMoon, Cislunar Explorer A, Cislunar Explorer B, CU-E3, Miles