Prisma is a satellite project led by the Swedish Space Corporation (SSC) which consist of two satellites that fly in formation.[1] Prisma is operated in collaboration with CNES, the French space agency, which provides the radiofrequency metrology system that enables the satellites to fly in close formation while autonomously avoiding collisions.[3]
![]() Prisma satellite during integration | |
Mission type | Technology demonstrator |
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Operator | Swedish National Space Board, DLR, CNES |
COSPAR ID | Mango: 2010-028B Tango: 2010-028F |
SATCAT no. | Mango: 36599 Tango: 36827 |
Mission duration | 1 year planned 12 years, 2 months and 1 day elapsed |
Spacecraft properties | |
Manufacturer | Saab Ericsson Space, Omnisys Instruments, ECAPS |
Launch mass | Mango: 145 kg (320 lb) Tango: 50 kg (110 lb) |
Dimensions | Mango: 80 cm × 130 cm (31 in × 51 in) Tango: 80 cm × 31 cm (31 in × 12 in) |
Power | Mango: 300 watts Tango: 90 watts |
Start of mission | |
Launch date | 15 June 2010, 14:42:16 UTC (2010-06-15UTC14:42:16Z)[1] |
Rocket | Dnepr rocket |
Launch site | Dombarovsky 370/13 |
Contractor | ISC Kosmotras |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Semi-major axis | 7,086 kilometres (4,403 mi)[2] |
Perigee altitude | 668.3 kilometres (415.3 mi)[2] |
Apogee altitude | 749 kilometres (465 mi)[2] |
Inclination | 98.4 degrees[2] |
Period | 99 minutes[2] |
Epoch | 24 March 2015, 11:08:39 UTC[2] |
It was launched, along with the PICARD spacecraft, on 15 June 2010 on a Dnepr launcher from Dombarovskiy Cosmodrome, near Yasny, Russia. Its primary objective is to test autonomous formation flying.[1][4] A secondary objective was to flight test a new monopropellant thruster using ammonium dinitramide (ADN) propellant.[5]
On 12 August 2010, SSC reported that the two satellites, called Mango and Tango, had separated from each other for the first time.[6]
← 2009 · Orbital launches in 2010 · 2011 → | |
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Compass-G1 | Globus-1M No.12L | Progress M-04M | STS-130 (Tranquility · Cupola) | SDO | Intelsat 16 | Kosmos 2459 · Kosmos 2460 · Kosmos 2461 | GOES 15 | Yaogan 9A · Yaogan 9B · Yaogan 9C | EchoStar XIV | Soyuz TMA-18 | STS-131 (Leonardo MPLM) | CryoSat-2 | GSAT-4 | Kosmos 2462 | USA-212 | SES-1 | Kosmos 2463 | Progress M-05M | STS-132 (Rassvet · ICC-VLD) | Akatsuki · IKAROS (DCAM-1 · DCAM-2) · Shin'en · Waseda-SAT2 · Hayato · Negai ☆'' | Astra 3B · COMSATBw-2 | USA-213 | SERVIS-2 | Compass-G3 | Badr-5 | Dragon Spacecraft Qualification Unit | STSAT-2B | Shijian XII | Prisma · Picard · BPA-1 | Soyuz TMA-19 | TanDEM-X | Ofek-9 | Arabsat-5A · Chollian | Progress M-06M | EchoStar XV | Cartosat-2B · AlSat-2A · StudSat · AISSat-1 · TIsat-1 | Compass-IGSO1 | Nilesat 201 · RASCOM-QAF 1R | Yaogan 10 | USA-214 | Tian Hui 1 | Kosmos 2464 · Kosmos 2465 · Kosmos 2466 | Chinasat-6A | Gonets-M No.2 · Kosmos 2467 · Kosmos 2468 | Progress M-07M | Michibiki | USA-215 | Yaogan 11 · Zheda Pixing 1B · Zheda Pixing 1C | USA-216 | Kosmos 2469 | Chang'e 2 | Shijian 6G · Shijian 6H | Soyuz TMA-01M | XM-5 | Globalstar 73 · Globalstar 74 · Globalstar 75 · Globalstar 76 · Globalstar 77 · Globalstar 79 | Progress M-08M | Eutelsat W3B · BSat 3B | Compass-G4 | Meridian 3 | Feng Yun 3B | COSMO-4 | SkyTerra-1 | STPSat-2 · RAX · O/OREOS · FASTSAT (NanoSail-D2) · FalconSat-5 · Sara-Lily · Emma | USA-223 | Chinasat-20A | Intelsat 17 · Hylas 1 | Glonass-M No.39 · Glonass-M No.40 · Glonass-M No.41 | SpaceX COTS Demo Flight 1 · Mayflower · SMDC-ONE 1 · QbX-1 · QbX-2 · Perseus 000 · Perseus 001 · Perseus 002 · Perseus 003 | Soyuz TMA-20 | Compass-IGSO2 | GSAT-5P | KA-SAT| Alsat-2A | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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