HIBARI (satellite)

In today's world, HIBARI (satellite) has become a topic of great relevance and interest to a wide range of people. From its origin to its impact on today's society, HIBARI (satellite) has sparked debates and reflections in different areas, and its influence extends to various aspects of daily life. In this article, we will explore in detail the various aspects related to HIBARI (satellite), analyzing its historical, social, cultural and economic dimensions. Through a multidisciplinary approach, we will seek to understand the complexity and importance of HIBARI (satellite) in the contemporary world, as well as its potential to generate significant changes in different spheres of society.

HIBARI
OperatorTokyo Institute of Technology
COSPAR ID2021-102F Edit this at Wikidata
SATCAT no.49400Edit this on Wikidata
Spacecraft properties
ManufacturerTokyo Institute of Technology
Launch mass55 kg (121 lb)
Dimensions50 × 50 × 50 cm (20 × 20 × 20 in)
Start of mission
Launch date9 November 2021, 00:55 UTC
RocketEpsilon (No. 5)
Launch siteUchinoura Space Center
ContractorJAXA
Orbital parameters
Reference systemGeocentric orbit (planned)
RegimeSun-synchronous orbit
Perigee altitude560 km (350 mi)
Apogee altitude560 km (350 mi)
Inclination97.6°
Instruments
Ultraviolet telescope
 

HIBARI is a space mission by Japan for a microsatellite that would test a new attitude control (orientation) method to achieve high accuracy pointing for its small telescope, and was launched on 9 November 2021 by an Epsilon launch vehicle as part of the Innovative Satellite Technology Demonstration Program-2 mission. The key technology to be tested on HIBARI is called "Variable Shape Attitude Control" (VSAC), and it is based on reaction torque by rotating its four solar array paddles.

Conceptual design

HIBARI is a space mission by the Japanese scientists from the Tokyo Institute of Technology to develop high pointing stability and agile maneuvering of a small satellite by using reaction torque of the satellite's structure. This technology, first presented in 2016, is hoped to substitute the use of reaction wheels and control moment gyroscopes (CMG), which arguably have difficulty achieving both agility and stability simultaneously. This capability would be useful for a very fast response to observe in the direction of gravitational waves or other transient astrophysical phenomena.

The spacecraft is a 55 kg (121 lb) microsatellite configured in a 50 cm (20 in) cube, where half of it would carry a small ultraviolet telescope to verify the pointing stability (< 10 𝑎𝑟𝑐𝑠𝑒𝑐2) and accuracy of the VSAC system. The orientation high accuracy would be achieved by rotating the arms of its four solar arrays in an orthogonal axis. Solar cells would be mounted on both sides of each of four solar array paddles.

References

  1. ^ イプシロンロケット5号機による革新的衛星技術実証2号機の打上げ結果について [Innovative satellite technology demonstration by Epsilon rocket No. 5 About the launch result of No. 2] (in Japanese). JAXA. 9 November 2021. Retrieved 9 November 2021.
  2. ^ a b c Variable Shape Attitude Control Demonstration with Microsat "HIBARI" Kenichi Sasaki, Yuhei Kikuya, Sho Koizumi, Yuto Masuda, Yusuke Shintani, Tsubasa Tsunemitsu, Takashi Furuya, Yohei Iwasaki, Yuichiro Takeuchi, Kei Watanabe, Saburo Matunaga Tokyo Institute of Technology 32nd Annual AIAA/USU Conference on Small Satellites 2018
  3. ^ a b c d Variable Shape Attitude Control Demonstration with Microsat "HIBARI" (Slide presentation) Kenichi Sasaki, Yuhei Kikuya, ShoKoizumi, YutoMasuda, ToshikiOzawa, Yusuke Shintani, Tsubasa Tsunemitsu, Yuichiro Takeuchi, Yoichi Yatsu, Saburo Matunaga Tokyo Institute of Technology 4 August 2018
  4. ^ A Study of Rest-to-Rest Three-Axis Attitude Maneuver with Shape Variable Function Watanabe Fuuta Tokyo Institute of Technology January 2016 doi:10.1299/jsmesec.2016.25.2B1
Wikious
Boobota
Sagapedia