Mission type | Education and Technology Demonstration |
---|---|
Operator | Delft University of Technology |
COSPAR ID | 2013-066N |
SATCAT no. | 39428 |
Website | www |
Mission duration | 10 years, 2 months, 13 days (in progress) |
Spacecraft properties | |
Spacecraft type | 3U CubeSat |
Manufacturer | Pumpkin, Inc |
Launch mass | 3 kilograms (6.6 lb) [1] |
Dimensions | 10 x 10 x 30 cm [1] |
Start of mission | |
Launch date | 21 November 2013, 07:10:16 UTC [2] |
Rocket | Dnepr |
Launch site | Dombarovsky 370/13 |
Contractor | Kosmotras |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 599 kilometres (372 mi) |
Apogee altitude | 780 kilometres (480 mi) |
Inclination | 97.76 degrees |
Period | 98.41 minutes |
Epoch | 24 May 2014, 14:04:39 UTC [3] |
Delfi-n3Xt is a Dutch nanosatellite which is operated by Delft University of Technology. [4] It was launched on 21 November 2013. [5] It is a three-unit CubeSat which will be used to demonstrate propulsion and communications systems for future missions. [6]
Delfi-n3Xt was launched successfully by a Dnepr carrier rocket flying from Site 370/13 at the Dombarovsky launch site. Delfi was a secondary payload aboard the rocket, whose primary mission was to deploy DubaiSat 2 and STSAT-3. Delfi was one of 25 secondary payloads aboard the rocket, for a total of 32 satellites.
The Delfi team made contact with the satellite during its first pass.
The Dnepr rocket was a space launch vehicle named after the Dnieper River. It was a converted ICBM used for launching artificial satellites into orbit, operated by launch service provider ISC Kosmotras. The first launch, on April 21, 1999, successfully placed UoSAT-12, a 350 kg demonstration mini-satellite, into a 650 km circular Low Earth orbit.
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