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.


PAN [Cornell University]

The PAN (Pathfinder for Autonomous Navigation) is a technology demonstration to launch two 3U CubeSats that will autonomously rendezvous and dock in low-Earth orbit.

The Pathfinder for Autonomous Navigation (PAN) project aims to launch two 3U+ CubeSats which will autonomously rendezvous and dock in Low Earth Orbit. This is the first CubeSat mission to ever attempt docking and will represent one of the most advanced autonomous CubeSat systems that has flown to date. Demonstrating autonomous rendezvous and docking capabilities on the CubeSat scale opens the door to new spaceflight capabilities such as the on-orbit assembly of advanced structures like space stations.

The project will demonstrate autonomous control algorithms for rendezvous and docking maneuvers; low-power reconfigurable magnetic docking technology; and compact, lightweight and inexpensive precision relative navigation using carrier-phase differential (CD) GPS. If successful, the technology demonstrated by PAN will reduce the mass and complexity associated with traditional rendezvous and docking systems.

PAN started as a collaboration between NASA’s Langley Research Center in Hampton, Virginia, and Cornell University. The team delivered two satellite prototypes to Langley in October 2016 for a ground demonstration to complete this phase of the project, and now the team plans to deliver two flight-ready satellites in early 2019 for launch shortly after.

It was selected in 2018 by NASA's CubeSat Launch Initiative (CSLI) to be launched as part of the ELaNa program.

PAN is planned to be launched 2019 on a LauncherOne rocket on the STP-27VP mission.

Nation: USA
Type / Application: Technology
Operator: Cornell University
Contractors: Cornell University
Equipment: Magnetic docking system
Configuration: CubeSat (3U)
Propulsion: 4 cold gas thrusters
Power: Solar cells, batteries
Lifetime: 4 months
Mass: 4.6 kg
Satellite COSPAR Date LS Launch Vehicle Remarks
PAN A 2022-003A ? 13.01.2022 Mo RW12/30 LauncherOne with PAN B, GEARRS 3, TechEdSat 13, ADLER 1, STORK 3, SteamSat 2
PAN B 2022-003C ? 13.01.2022 Mo RW12/30 LauncherOne with PAN A, GEARRS 3, TechEdSat 13, ADLER 1, STORK 3, SteamSat 2


Cite this page: