Hodoyoshi 4
id:
hodoyoshi-4-182-11650622
title:
Hodoyoshi 4
text:
Hodoyoshi-4 is a Japanese micro-satellite launched in 2014. The satellite is built in 0.5x0.6x0.7m 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 "miniature" ion thruster with specific impulse of 1100 s and operating power of 20 W is integrated into the body. The satellite was developed under the Funding Program for World-Leading Innovation R
brand slug:
wiki
category slug:
encyclopedia
description:
Japanese micro-satellite launched in 2014
original url:
https://en.wikipedia.org/wiki/Hodoyoshi_4
date created:
2014-06-24T01:51:15Z
date modified:
2024-09-06T09:36:38Z
main entity:
{"identifier":"Q17285879","url":"https://www.wikidata.org/entity/Q17285879"}
image:
fields total:
13
integrity:
15