Demonstrator of Atmospheric Reentry System and Hypervelocity
spacecraft used to test reentry systems for the Hayabusa probe, failed to separate from launch vehicle
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Demonstrator of Atmospheric Reentry System and Hypervelocity
Summary
Demonstrator of Atmospheric Reentry System and Hypervelocity is a microsatellite[1]. It is known by 3 alternative names across languages and contexts.[2]
Key Facts
- Demonstrator of Atmospheric Reentry System and Hypervelocity's instance of is recorded as microsatellite[3].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's COSPAR ID is recorded as 2002-003B[4].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's space launch vehicle is recorded as H-IIA[5].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's SCN is recorded as 27368[6].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's UTC date of spacecraft launch is recorded as +2002-02-04T00:00:00Z[7].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's significant event is recorded as rocket launch[8].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's start point is recorded as Yoshinobu Launch Complex Launch Pad 1[9].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's mass is recorded as {'unit': 'Q11570', 'amount': '+89'}[10].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's Google Knowledge Graph ID is recorded as /g/122043nr[11].
- Demonstrator of Atmospheric Reentry System and Hypervelocity's NSSDCA ID is recorded as 2002-003B[12].
Why It Matters
Demonstrator of Atmospheric Reentry System and Hypervelocity is known by 3 alternative names across languages and contexts.[2]