Session

Technical Poster Session 10: Propulsion

Location

Utah State University, Logan, UT

Abstract

THE MISSION

Launch date: 07 November 2021

Object name: R2

NORAD-ID: 46913

Platform: design based on the M6P platform

Size: 6U

Manufacturer: NanoAvionics

Payloads: from Exotrail - a high-thrust, electrical Hall Effect Thruster - and a RF payload

LAUNCH PARAMETERS

Altitude: 571 km - Inclination: 36.9° - Eccentricity: 0.001

GROUND STATION NETWORKS

  • Due to the low inclination, NanoAvionics-owned stations do not have visibility
  • Leaf Space provided communication through their Leaf Line GSaaS with stations in Italy and in New-Zealand

MISSION OBJECTIVES FOR THE THRUSTER PAYLOAD

  • Main objective: configure the thruster for a firing and perform an ignition with nominal parameters.
  • Bonus: Perform altitude change significant enough to validate orbit phasing and plane change.

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Aug 7th, 12:00 AM

Operational Challenges and Experience Learnt from Operating a Satellite with High-Thrust Electric Propulsion

Utah State University, Logan, UT

THE MISSION

Launch date: 07 November 2021

Object name: R2

NORAD-ID: 46913

Platform: design based on the M6P platform

Size: 6U

Manufacturer: NanoAvionics

Payloads: from Exotrail - a high-thrust, electrical Hall Effect Thruster - and a RF payload

LAUNCH PARAMETERS

Altitude: 571 km - Inclination: 36.9° - Eccentricity: 0.001

GROUND STATION NETWORKS

  • Due to the low inclination, NanoAvionics-owned stations do not have visibility
  • Leaf Space provided communication through their Leaf Line GSaaS with stations in Italy and in New-Zealand

MISSION OBJECTIVES FOR THE THRUSTER PAYLOAD

  • Main objective: configure the thruster for a firing and perform an ignition with nominal parameters.
  • Bonus: Perform altitude change significant enough to validate orbit phasing and plane change.