Aalto-1

Aalto-1
Aalto-1 flight model in March 2016.
Mission typeTechnology demonstration
OperatorAalto University
COSPAR ID2017-036L Edit this at Wikidata
SATCAT no.42775
Websitewiki.aalto.fi/display/SuomiSAT/Aalto-1+nanosatellite+project
Mission duration2 years (planned)
6 years, 11 months and 13 days (in progress)
Spacecraft properties
Spacecraft typeCubeSat
Bus3U CubeSat
ManufacturerAalto University
Launch mass4 kg (8.8 lb)
Dimensions10 × 10 × 34 cm (3.9 × 3.9 × 13.4 in)
Power4.8 watts
Start of mission
Launch date23 June 2017, 03:59 UTC
RocketPolar Satellite Launch Vehicle (PSLV-C38)
Launch siteSatish Dhawan Space Centre, First Launch Pad (FLP)
ContractorIndian Space Research Organisation
Entered service24 July 2017 (first image)
Orbital parameters
Reference systemGeocentric orbit
RegimeLow Earth orbit
Perigee altitude505 km (314 mi)
Apogee altitude505 km (314 mi)
Inclination97.44°
Period90.0 minutes
Instruments
Imaging Fabry-Pérot Spectrometer
Compact Radiation Monitor
Electrostatic Plasma Brake
Aalto-2 →
 
Artist's impression of Aalto-1 releasing its electrostatic plasma brake tether.

Aalto-1 is a Finnish research nanosatellite, created by students of Aalto University. Based on the CubeSat architecture, it was originally scheduled to be launched in 2013, it was launched on 23 June 2017. It is Finland's first student satellite project and indigenously produced satellite.[1] As of 2021, the satellite is operational.[2]

  1. ^ "The Finnish student satellite project". aalto1.fi. 8 May 2017. Retrieved 25 May 2017.
  2. ^ "Mission and Science Results". Aalto University. 1 July 2021. Retrieved 26 October 2021.

© MMXXIII Rich X Search. We shall prevail. All rights reserved. Rich X Search