Shin'en [UNISEC]
Shin'en 2 is a interplanetary satellite built by students at Kyushu Institute of Technology and Kagoshima University, AUT in Japan that carries a 145 to 435 MHz linear transponder into a deep space heliocentric orbit.
The 15 kg spacecraft, measuring 490 × 490 × 475 mm, features a lightwight thermoplastic CFRP structure. It is powered by solar cells on the polyheadral surface of the satellite body. Shin'en 2 will orbit the Sun in an elliptic orbit between Venus and Mars. Its inclination will be almost zero, which means Shin'en 2 will stay in the Earth’s equatorial plane. The distance from the Sun will be between 0.7 and 1.3 AU.
The goals of the mission are:
Shin'en 2 is planned to launch in the 4th quarter of 2014 on an H-2A-202 rocket with Hayabusa 2 as the main payload and PROCYON and ARTSAT2:DESPATCH as secondary payloads.
After launch, Shin'en 2 got the additional designation Fuji OSCAR 82 (FO 82).
Nation: | Japan |
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Type / Application: | Technology, interplanetary |
Operator: | Kyushu Institute of Technology, Kagoshima University, AUT |
Contractors: | Kyushu Institute of Technology, Kagoshima University, AUT |
Equipment: | |
Configuration: | |
Propulsion: | None |
Power: | Solar cells, batteries |
Lifetime: | ? |
Mass: | 15 kg |
Orbit: | 0.7 AU × 1.3 AU, ~0° heliocentric orbit |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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Shin'en 2 (FO 82, Fuji-OSCAR 82) | 2014-076B | 03.12.2014 | Ta YLP-1 | H-2A-202 | with Hayabusa 2, PROCYON, DESPATCH |