Mission type | Technology demonstration |
---|---|
Operator | Aalto University |
COSPAR ID | 2017-036L |
SATCAT no. | 42775 |
Website | wiki |
Mission duration | 2 years (planned) 6 years, 3 months and 15 days (in progress) |
Spacecraft properties | |
Spacecraft type | CubeSat |
Bus | 3U CubeSat |
Manufacturer | Aalto University |
Launch mass | 4 kg (8.8 lb) |
Dimensions | 10 × 10 × 34 cm (3.9 × 3.9 × 13.4 in) |
Power | 4.8 watts |
Start of mission | |
Launch date | 23 June 2017, 03:59 UTC |
Rocket | Polar Satellite Launch Vehicle (PSLV-C38) |
Launch site | Satish Dhawan Space Centre, First Launch Pad (FLP) |
Contractor | Indian Space Research Organisation |
Entered service | 24 July 2017 (first image) |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Low Earth orbit |
Perigee altitude | 505 km (314 mi) |
Apogee altitude | 505 km (314 mi) |
Inclination | 97.44° |
Period | 90.0 minutes |
Instruments | |
Imaging Fabry-Pérot Spectrometer Compact Radiation Monitor Electrostatic Plasma Brake | |
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]
The Aalto-1 project began in 2010 with a feasibility study, which was conducted as part of a university course on space technology. [3] The study was followed by the publication of a preliminary design in 2011. [3] A critical design review (CDR) of the satellite was conducted in 2012. [3] In all, over 80 students of Aalto University's School of Electrical Engineering were involved in the project. [4]
The solar-powered CubeSat – based satellite will weigh approximately 4 kg (8.8 lb), [3] and has 3 main payloads: a miniature Fabry-Pérot spectrometer, designed by VTT Technical Research Centre, [5] a RADMON-radiation detector developed by University of Helsinki and University of Turku for the study of solar wind conditions in the Earth orbit (and to study the radiation environment in general), and an electric sail (dubbed a "brake tether"), which is designed for an atmospheric entry at the end of its 2-year operational lifespan, [6] with the intent of avoiding the creation of space junk. [3]
Originally the satellite was to be launched by a Falcon 9 launch vehicle, but the launcher suffered multiple delays due to the accidents that plagued the Falcon 9 in 2015 and 2016. The launch was removed from the Falcon 9, and Aalto-1 was launched on 23 June 2017 by PSLV-C38 launch vehicle from India.
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