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]
![]() Aalto-1 flight model in March 2016. | |
Mission type | Technology demonstration |
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Operator | Aalto University |
COSPAR ID | 2017-036L ![]() |
SATCAT no. | 42775 |
Website | wiki |
Mission duration | 2 years (planned) 4 years, 11 months and 26 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 nanosatellite Series Aalto-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.
← 2016 · Orbital launches in 2017 · 2018 → | |
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January | TJS-2 – Lingqiao / Jilin-1 03 · Caton-1 · Xingyun Shiyan 1 – Iridium NEXT 1–10 – TRICOM-1 – USA-273 / SBIRS GEO-3 – DSN-2 – Hispasat AG1 |
February | Intelsat 32e / SkyBrasil1 · Telkom-3S – Cartosat-2D · INS-1A, 1B · Flock-3p × 88 · Lemur-2 × 8 · Al Farabi-1 · BGUSAT · DIDO-2 · Nayif 1 · PEASS – Dragon CRS-10 – Progress MS-05 |
March | USA-274 / NROL-79 / Intruder 8 – Tiankun-1 – Sentinel-2B – EchoStar 23 – IGS-Radar 5 – USA-275 / WGS-9 – SES-10 |
April | Shijian 13 – Cygnus CRS OA-7 · (ALTAIR · CXBN-2 · IceCube · SG-Sat · SHARC) – Soyuz MS-04 – Tianzhou 1 · SilkRoad-1 |
May | USA-276 / NROL-76 – Koreasat 7 · SGDC-1 – GSAT 9 / South Asia Satellite – Inmarsat-5 F4 – SES-15 – "It's a Test" – EKS-2 |
June | QZS-2 – ViaSat-2 · Eutelsat 172B – Dragon CRS-11 · NICER · Birds-1 (TOKI · GhanaSat-1 · Mazaalai · BRAC Onnesha · Nigeria EduSat-1) – GSAT-19 – EchoStar 21 – Progress MS-06 – HXMT / Insight · Zhuhai-1 01, 02 · ÑuSat 3 – ChinaSat 9A – Cartosat-2E · Aalto-1 · ROBUSTA-1B · Max Valier Sat – Nivelir-ZU (14F150) – BulgariaSat-1 – Iridium NEXT-2 – EuropaSat/Hellas Sat 3 · GSAT-17 |
July | Shijian-18 – Intelsat 35e – Kanopus-V-IK · CICERO × 3 · Corvus-BC × 2 · Ecuador-UTE-YuZGU · Flock-2k × 48 · Flying Laptop · Iskra-MAI-85 · Lemur-2 × 8 · MKA-N × 2 · Mayak · NORSAT-1, -2 · NanoACE · TechnoSat · WNISAT-1R – Soyuz MS-05 |
August | OPTSAT-3000 · VENµS – Dragon CRS-12 · ASTERIA – Blagovest 11L – TDRS-M – Michibiki 3 – Formosat-5 – ORS-5 – IRNSS-1H |
September | USA-277 / OTV-5 – Amazonas 5 – Soyuz MS-06 – Kosmos 2522 / GLONASS-M 752 – USA-278 / NROL-42 – AsiaSat 9 – Yaogan-30-01 × 3 – Intelsat 37e · BSAT-4a |
October | VRSS-2 – Iridium NEXT 21–30 – QZS-4 – SES-11 / EchoStar 105 – Sentinel-5 Precursor – Progress MS-07 – USA-279 / NROL-52 / Quasar 21 – Koreasat 5A – SkySat × 6 · Flock-3m × 4 |
November | BeiDou-3 M1 · M2 – Mohammed VI-A – Cygnus CRS OA-8E · Asgardia-1 – Fengyun-3D · HEAD-1 – NOAA-20 – Jilin-1 × 3 – Yaogan-30-02 × 3 – Meteor-M No.2-1 |
December | Kosmos 2524 – LKW-1 – Alcomsat-1 – Galileo FOC 15-18 – Dragon CRS-13 – Soyuz MS-07 – GCOM-C · SLATS – Iridium NEXT 31–40 – Yaogan-30-03 × 3 – AngoSat 1 |
Launches are separated by dashes ( – ), payloads by dots ( · ), multiple names for the same satellite by slashes ( / ). CubeSats are smaller. Crewed flights are underlined. Launch failures are in italics. Payloads deployed from other spacecraft are (enclosed in brackets). |