Double Star 2
former joint Chinese-European magnetospheric research satellite
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Double Star 2
Summary
Double Star 2 is a geomagnetic satellite[1]. It is known by 5 alternative names across languages and contexts.[2]
Key Facts
- Double Star 2's instance of is recorded as geomagnetic satellite[3].
- Double Star 2's instance of is recorded as former entity[4].
- Double Star 2's operator is recorded as China National Space Administration[5].
- Double Star 2's operator is recorded as European Space Agency[6].
- Double Star 2's manufacturer is recorded as China Academy of Space Technology[7].
- Double Star 2's COSPAR ID is recorded as 2004-029A[8].
- Double Star 2's part of is recorded as Double Star mission[9].
- Double Star 2's space launch vehicle is recorded as Long March 2C[10].
- Double Star 2's SCN is recorded as 28382[11].
- Double Star 2's country of origin is recorded as People's Republic of China[12].
- Double Star 2's powered by is recorded as spacecraft solar array[13].
- Double Star 2's powered by is recorded as nickel–hydrogen battery[14].
- Double Star 2's UTC date of spacecraft launch is recorded as +2004-07-25T00:00:00Z[15].
- Double Star 2's significant event is recorded as rocket launch[16].
- Double Star 2's significant event is recorded as failure[17].
- Double Star 2's start point is recorded as Taiyuan Satellite Launch Center[18].
- Double Star 2's height is recorded as {'unit': 'Q11573', 'amount': '+1.4'}[19].
- Double Star 2's mass is recorded as {'unit': 'Q11570', 'amount': '+330'}[20].
- Double Star 2's diameter is recorded as {'unit': 'Q11573', 'amount': '+2.1'}[21].
- Double Star 2's Wolfram Language entity code is recorded as Entity["Satellite", "28382"][22].
- Double Star 2's NSSDCA ID is recorded as 2004-029A[23].
Why It Matters
Double Star 2 is known by 5 alternative names across languages and contexts.[2]