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From Wikipedia, the free encyclopedia

OPUSAT
Mission typeTechnology
OperatorOsaka Prefecture University
COSPAR ID2014-009D
SATCAT no.39575
Websitewww.sssrc.aero.osakafu-u.ac.jp/E_SSSRC_HP/projects/OPUSAT/home.html
Spacecraft properties
Spacecraft type1U CubeSat
ManufacturerOsaka Prefecture University
Launch mass1.4 kilograms (3.1 lb)
Start of mission
Launch date27 February 2014, 18:37 (2014-02-27UTC18:37Z) UTC[1]
RocketH-IIA 202
Launch siteTanegashima Yoshinobu 1
ContractorMitsubishi
End of mission
Decay date24 July 2014 (2014-07-25)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude383 kilometres (238 mi)
Apogee altitude389 kilometres (242 mi)
Inclination65 degrees
Period92.27 minutes
Epoch28 February 2014[2]
 

The Osaka Prefecture University Satellite, or OPUSAT was a technology demonstration cubesat built and operated by Japan's Osaka Prefecture University. It had a size of 100x100x100mm (without antennas and solar paddles) and build around a standard 1U cubesat bus. The primary satellite purpose is the space testing of the power system based on a Lithium-ion capacitor. The tests were largely successful,[3] and it finished operation by reentry to Earth atmosphere on 24 July 2014. The OPUSAT is a development successor to “Maido Ichigo” satellite by East Osaka Craftmen Astro-Technology SOHLA in Osaka.

See also

References

  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 1 January 2015.
  2. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 1 January 2015.
  3. ^ "OPUSAT achieved minimum mission success". SSSRC (in Japanese). May 4, 2014. Archived from the original on September 29, 2013. Retrieved June 16, 2014.

External links


This page was last edited on 20 February 2021, at 15:54
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