Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

PROCYON

PROCYON [JAXA]

PROCYON (Proximate Object Close flyby with Optical Navigation) is an experimental asteroid fly-by probe developed by JAXA.

The probe with a mass of only 59 kg was to perform an close fly-by to an asteroid by using optical navigation. Two more asteroid fly-bys were planned.

The probe was to demonstrate several technologies of 50 kg deep space exploration bus sytem:

  • power generation, thermal control, attitude control, communication, orbit determination in deep space,
  • orbit control by small electric propulsion system
  • communication using high-efficiency GaN X-band
  • power amplifier
  • Precise DDOR navigation in deep space
  • optical navigation to encounter asteroid
  • asteroid close flyby observation

PROCYON was launched in mid 2014 on a H-2A-202 rocket with the asteroid explorer Hayabusa 2 as the main payload. The target asteroid for PROCYON is 2000 DP107, which has small moon.

PROCYON's ion engine has operated for more than 223 hours in total. Thrust is 366 µN, more than the specification of 300 µN. The ion engine's high voltage power trouble is the most problematic situation, which might be caused by small metal debris. If the problem is not resolved end of April 2015, the planned Earth fly-by on 3 December 2015 and the asteroid fly-by observation on 12 May 2016 will be difficult. In early May 2015, the plans to visit asteroid (185851) 2000 DP107 were abandoned after recovery of ion thrusters failed.

Nation: Japan
Type / Application: Asteroid fly by probe
Operator: JAXA
Contractors:
Equipment:
Configuration:
Propulsion: 300 µN ion engine
Power: 4 deployable fixed solar arrays, batteries
Lifetime:
Mass: 59 kg
Orbit: Heliocentric
Satellite COSPAR Date LS Launch Vehicle Remarks
PROCYON 2014-076D 03.12.2014 Ta YLP-1 H-2A-202 with Hayabusa 2, DESPATCH, Shin'en 2