AuroraSat

In-Orbit Demonstration mission. SatRevolution S. A. provides a satellite platform based on 1.5U bus for Aurora Propulsion Technologies payload. Launch is planned on December 2020 with SpaceX Falcon 9 rocket.
ico-amicalsat-01

CubeSat based demonstration mission

ico-kraksat-01

Attitude and orientation control Proof of Concept

ico-amicalsat-03

International co-development project with Finnish company Aurora Propulsion Technologies 

For more information please visit Aurora Propulsion Technologies website.

Subsystems

Plasma Brake Module (PBM):
  • Lightweight deorbiting system
  • capable of deorbiting up to 1000kg satellite from 1000km
  • Low power consumption required
Attitude and Orbit Control system (AOCS):
  • Resistojet propulsion module
  • Water-based propellant
  • Capable of attitude adjustments and orbital control maneuvers
  • 12 individual thrusters
  • Main processor: MSP430FR5994
  • 16 MHz, 2 MB MRAM 256 KB FRAM,
  • Ultra Low-Power Modes
  • 2 × UHF & S-band
  • UHF operational frequency 435-438 MHz
  • S-band operational frequency 2400-2450 GHz
  • UHF transmission data rate 9,6 kb/s (option for 64 kb/s)
  • S-band transmission rate 0,5 Mb/s
  • Range 400-500 km
  • Orientation accuracy: ~2 deg
  • Maximum random offset below 0,5 deg/s/axis
  • Payload power output: 0,5 W
  • Open circuit voltage: 6,3 V
  • Solar panels efficiency 22%
  • 1.5U Structure
  • CNC manufactured of Aluminium 7075 alloy
  • Hard anodized and oxidized

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HQ

Stabłowicka 147
54-066 Wrocław
Poland

U.S. Office

388 Market Street (Suite 1300)
San Francisco, CA 94111
United States

+48 533 325 851
contact@satrevolution.com