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.
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.