Delfi-C3
| Delfi-C3 | |
|---|---|
 | |
| Position | デルフト college of engineering |
| Satellite bus | CubeSat 3 U [1] |
| Duty | Technical proof |
| The launching date and time | 2008-04-28 |
| Transportation rocket | PSLV-CA (C-9) |
| Launching place | サティシュ ダワン space center |
| COSPAR ID | 2008-021G |
| Official site | Delfi-C3 - Home |
| Mass | 2.2 kg |
| Power consumption | 2.5 W |
| Battery | Unavailable |
| Orbital element | |
| Orbit | Low orbit |
CubeSat where Netherlands デルフト techie made Delfi-C3.
With a CubeSat-3U type [1], it was launched as part of NLS-4 mission [2] on April 28, 2008 by Indian PSLV rocket [3]. The launching of Delfi-C3 was contracted with an Indian space research engine through Antrix company and UTIAS [2].
The main mission of the satellite is technical proof and development [4]. It was equipped with a new solar battery, sun sensor of TNO, a high efficiency transceiver [4].
In addition, battery is not put on Delfi-C3, and is active, posture controlling it does not go.
In addition, this satellite is ANS, IRAS, a man-made satellite of the Netherlands fourth plane next to SLOSHSAT and is the satellite with the Netherlands first university.
References
Allied item
This article is taken from the Japanese Wikipedia Delfi-C3
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