Prisma satellite during integration | |
Mission type | Technology demonstrator |
---|---|
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 9 years, 10 months and 25 days 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[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] |
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]
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]
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