Hodoyoshi 3
id:
hodoyoshi-3-182-7388208
title:
Hodoyoshi 3
text:
Hodoyoshi-3 is a Japanese micro-satellite launched in 2014. The satellite is built in 0.5x0.5x0.65m box-shape bus, optimized for piggy-back launch.
All instruments are powered by solar cells mounted on the spacecraft body and two stub wings, with estimated electrical power of 50W. For orbit-keeping, a hydrogen peroxide thruster is used. The satellite was developed under the Funding Program for World-Leading Innovation R&D on Science and Technology.
brand slug:
wiki
category slug:
encyclopedia
description:
Japanese micro-satellite launched in 2014
original url:
https://en.wikipedia.org/wiki/Hodoyoshi_3
date created:
2014-06-24T03:58:27Z
date modified:
2024-09-06T09:20:16Z
main entity:
{"identifier":"Q17285875","url":"https://www.wikidata.org/entity/Q17285875"}
image:
fields total:
13
integrity:
15