FUNcube-1
![]() FUNcube-1 in the cleanroom | |
Mission type | Amateur Radio |
---|---|
Operator | AMSAT-UK |
COSPAR ID | 2013-066AE ![]() |
SATCAT no. | 39444 |
Website | funcube.org.uk |
Mission duration | 10 years, 11 months and 5 days elapsed |
Spacecraft properties | |
Bus | 1U CubeSat[1] |
Manufacturer | ISIS-BV, AMSAT-NL, AMSAT-UK |
Launch mass | 0.98 kilograms (2.2 lb) |
Power | 2.2 watts |
Start of mission | |
Launch date | 21 November 2013 (2013-11-21) |
Rocket | Dnepr |
Launch site | Yasny Launch Base |
Contractor | ISL |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 592.6 kilometers (368 Mi) |
Apogee altitude | 678.6 kilometers (421 Mi) |
Inclination | 97.7 Degrees |
Period | 97.3 Minutes |
FUNcube-1 is a complete educational single unit CubeSat satellite with the goal of enthusing and educating young people about radio, space, physics and electronics. It is part of a program which aims to launch more of these educational CubeSats.[1] It is the first satellite with outreach as its primary mission.
FUNcube project
Project
The FUNcube project was started in the UK by AMSAT-UK. The satellite has been developed by a team of volunteers from AMSAT-UK and AMSAT-NL, and was assembled at ISIS in Delft. It has been designated with OSCAR number 73 by AMSAT and is now also known as AO-73.
Mission
As part of its mission, FUNcube-1 carries a materials science experiment, from which the school students can receive telemetry data and which they can compare to the results they obtained from similar reference experiments in the classroom. This experiment resembles the Leslie's Cube experiment. One of the first schools to use FUNcube-1 in the classroom was Abbeys Primary School in Bletchley which also featured in the BBC breakfast news two days after launch.[2]
Satellite
Instruments
FUNcube-1 is equipped with a UHF to VHF linear transponder with approx 300 mW PEP output and which can be used by Radio Amateurs worldwide for SSB and CW communications during the weekends.
Specifications
Frequencies:
- Telemetry down link 145.935 MHz 1200bd BPSK with FEC
- Transponder Uplink 435.150 - 435.130 MHz LSB (Inverting)
- Downlink 145.950 - 145.970 MHz USB
Maximum uplink power of 5 watts to a 7 dBi gain antenna, more power is not needed to use the transponder. Transponder is SSB/CW Inverting.
Launch
FUNcube-1 was launched at 07:10:11 UTC on 21 November 2013,[3][4][5] as part of the ISILaunch03 campaign,[6] aboard a Dnepr rocket, from Yasny Launch Base, Russia. The launch was contracted by ISL, and operated by ISC Kosmotras.
Distribution
The FUNcube distributed ground station network (DGSN) is used in which radio amateurs receive packets and send these via the internet to the central data collection server, called the data warehouse.
To enable easy reception, one of the FUNcube team members, Howard Long G6LVB, has created a USB connected receiver called the FUNcube Dongle.
See also
References
External links
- funcube.org.uk
- amsat-uk.org
- amsat-nl.org
- FUNcube Data Warehouse
- v
- t
- e
- Intelsat 27
- Globalstar M078, M087, M093, M094, M095, M096
- Azerspace-1/Africasat-1a, Amazonas 3
- Progress M-18M
- Landsat 8
- SARAL, Sapphire, NEOSSat, UniBRITE-1, TUGSAT-1, AAUSat-3, STRaND-1
- Anik G1
- Bion-M No.1 (Aist 2, BeeSat-2, BeeSat-3, SOMP, Dove-2, OSSI-1)
- Cygnus Mass Simulator, Dove 1, Alexander, Graham, Bell
- Progress M-19M
- Gaofen 1, TurkSat-3USat, NEE-01 Pegaso, CubeBug-1
- Kosmos 2485
- IRNSS-1A
- Uragan-M 48, 49, 50
- Shijian XI-05
- MUOS-2
- Shijian 15, Shiyan 7, Chuangxin 3
- Inmarsat-4A F4, INSAT-3D
- Progress M-20M
- Kounotori 4 (TechEdSat-3, ArduSat-1, ArduSat-X, PicoDragon)
- USA-244
- Arirang-5
- USA-245
- Eutelsat 25B / Es'hail 1, GSAT-7 / INSAT-4F
- Amos-4
- Yaogan 17 A, B, C
- LADEE
- Gonets-M No.5, Gonets-M No.6, Gonets-M No.7
- Hisaki
- USA-246
- Cygnus Orb-D1
- Fengyun III-03
- Kuaizhou-1
- Soyuz TMA-10M
- CASSIOPE, CUSat, POPACS 1, 2, 3, DANDE
- Astra 2E
- Shijian 16
- Sirius FM-6
- Yaogan 18
- Mars Orbiter Mission
- Soyuz TMA-11M
- Globus-1M No.13L
- MAVEN
- ORS-3, STPSat-3, Black Knight 1, CAPE-2, ChargerSat-1, COPPER, DragonSat-1, Firefly (satellite), Ho'oponopono-2, Horus, KySat-2, NPS-SCAT, ORSES, ORS Tech 1, 2, PhoneSat 2.4, Prometheus × 8, SENSE A, B, SwampSat, TJ3Sat, Trailblazer-1, Vermont Lunar CubeSat
- Yaogan 19
- DubaiSat-2, STSAT-3, SkySat-1, UniSat-5 (Dove 4, ICube-1, HumSat-D, PUCP-Sat 1 (Pocket-PUCP), BeakerSat-1, $50SAT, QBScout-1, WREN), AprizeSat 7, 8, Lem, WNISat-1, GOMX-1, CubeBug-2, Delfi-n3Xt, Dove 3, First-MOVE, FUNcube-1, HINCube-1, KHUSat-1, KHUSat-2, NEE-02 Krysaor, OPTOS, Triton 1, UWE-3, VELOX-P2, ZACUBE-1, BPA-3
- Swarm A, B, C
- Shiyan 5
- Progress M-21M
- Chang'e 3 (Yutu)
- SES-8
- USA-247 / Topaz, TacSat-6
- Inmarsat-5 F1
- CBERS-3†
- Gaia
- Túpac Katari 1
- Kosmos 2488 / Strela-3M 7, Kosmos 2489 / Strela-3M 8, Kosmos 2490 / Strela-3M 9, Kosmos-2491
- Ekspress AM5
- Aist 1, Kosmos 2491 / SKRL-756 1, Kosmos 2492 / SKRL-756 2
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).