Index
I Innovative Satellite Technology Demonstration Program
PurposeOutline of the Public Recruitment System
Previous Projects

II Innovative Satellite Technology Demonstration-3
Outline

02
02
02
02
03
03

RApid Innovative payload demonstration SatellitE-3 (RAISE-3)
Mission and Features of “RApid Innovative payload demonstration SatellitE-3

04
04

Satellite Systems

05

RAISE-3 Configuration

05

Main Characteristics

06

Configuration

07

Theme of on-orbit demonstration
01 Low Earth Orbit satellite MIMO for 920MHz band IoT platform “LEOMI”
02 Software Defined Receiver “SDRX”
03 cots GPU based Edge-computing for mission systems utilizing model based systems engineering “GEMINI”
04 Kakushin-3 water Ion-thruster and Resistojet-thruster “KIR”
05 Tokyo Metropolitan University Pulsed-Plasma Thruster “TMU-PPT”
06 Membrane deployment deorbit mechanism “D-SAIL”
07 Harvesting Energy with Lightweight Integrated Origami Structure “HELIOS”

08
08
09
09
09
10
10

Equipment that increases added value of mission
01 On Board Computer slice

11

Operation

11

RAISE-3 System Overview

12

Microsatellite [ Theme of on-orbit demonstration ]01 KOYOH
02 Platform for Extra and Terrestrial Remote Examination with LCTF “PETREL”
03 Space Tethered Autonomous Robotic Satellite “STARS-X”

13
13
14

CubeSat [ Theme of on-orbit demonstration ]01 MAGnetically separating NAno-satellite with Rotation for Orbit control “MAGNARO”
02 MITSUBA
03 KOSEN-2
04 WASEDA-SAT-ZERO
05 FSI-SAT

III Innovative Satellites

01 | Innovative Satellite Technology Demonstration-3

15
15
16
16
16
17

Innovative Satellite Technology Demonstration Program

Innovative Satellite Technology
Demonstration Program

Innovative Satellite Technology Demonstration-3

PurposeThis program is part of the basic plan for space policy to realize a comprehensive
industrial base in outer space to provide opportunities to demonstrate equipment, parts,
microsatellites and CubeSats developed by private companies, universities, research
institutions, etc.
JAXA is aiming to realize the following through this program.

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Outline of the Public Recruitment System
JAXA is offering proposals for “Innovative Satellite Technology Demonstration
Program” throughout the year. For details of application conditions etc, please see thefollowing website.

Microsatellite

未宇
来宙
をを
つ つ
くか
るう

(RAISE-3)[ 2 ] Although the risk is high, we will preferentially take “innovative” technologies that are expected to achieve highresults in the development of Japanese space technology and securing the international competitiveness of thespace industry and demonstrate.

RApid Innovative payload demonstration SatellitE-3[ 1 ] We will look forward to the future and demonstrate technologies and ideas that will lead to the creation of newuses and industrial competitive systems / subsystems while responding to the challenges of the country and industry.

詳しくはこちら ➡ https://www.kenkai.jaxa.jp/kakushin/

Innovative Satellite Technology Demonstration Program ( Japanese only )https://www.kenkai.jaxa.jp/kakushin/index.html

Innovative Satellite Technology Demonstration-1

Innovative Satellite Technology
Demonstration-2( Japanese only )Innovative Satellite Technology Demonstration-3 | 02

Innovative Satellites

Innovative Satellite Technology
Demonstration-1( Japanese only )Innovative Satellite Technology Demonstration-2

CubeSatPrevious Projects

Innovative Satellite Technology Demonstration Program

Innovative Satellite Technology
Demonstration-3

Innovative Satellite Technology Demonstration-3

OutlineThe “Innovative Satellite Technology Demonstration-3” is the third
demonstration opportunit y of the ” Innovative Satellite Technology
Demonstration Program” to publicly invite universities, research institutions,private companies, etc., equipped with 15 selected themes.
It consists of 9 satellites, “RApid Innovative payload demonstration
SatellitE-3” developed by JAXA entrusted to Mitsubishi Heavy Industries,
Ltd. (with 7 demonstration themes) and 8 microsatellites / CubeSats.

(RAISE-3)

RApid Innovative payload demonstration SatellitE-3

RApid Innovative payload demonstration SatellitE-3

RAISE-3 To be launched by Epsilon Launch Vehicle No.6
01 Low Earth Orbit satellite MIMO for 920MHz band IoT platform “LEOMI”
02 Software Defined Receiver “SDRX”
03 cots GPU based Edge-computing for mission systems utilizing model based
systems engineering “GEMINI”

04 Kakushin-3 water Ion-thruster and Resistojet-thruster “KIR”
05 Tokyo Metropolitan University Pulsed-Plasma Thruster “TMU-PPT”
Microsatellite

06 Membrane deployment deorbit mechanism “D-SAIL”
07 Harvesting Energy with Lightweight Integrated Origami Structure “HELIOS”

CubeSat To be launched by Epsilon Launch Vehicle No.6
02 MITSUBA
04 WASEDA-SAT-ZERO
01 MAGnetically separating NAno-satellite with Rotation for Orbit control“MAGNARO”
CubeSat

03 KOSEN-2
05 FSI-SAT

Multiple Satellite Mounting Structure

Microsatellite Launch vehicle is under adjusting
Innovative Satellites

01 KOYOH
02 Platform for Extra and Terrestrial Remote Examination with LCTF “PETREL”
03 Space Tethered Autonomous Robotic Satellite “STARS-X”
KOYOH

03 | Innovative Satellite Technology Demonstration-3

PETRELSTARS-X

Innovative Satellite Technology Demonstration Program

RApid Innovative payload demonstration
SatellitE-3 ( RAISE-3 )Innovative Satellite Technology Demonstration-3

Mission and Features of“RApid Innovative payload demonstration SatellitE-3 (RAISE-3)”(RAISE-3)

RApid Innovative payload demonstration SatellitE-3

MissionMicrosatellite

RAISE-3 (RApid Innovative payload demonstration SatellitE-3) is a satellite for seven on-orbit demonstration themes selected inthe "Innovative Satellite Technology Demonstration Program". RAISE-3 will be operated at the request of the proposers of eachtheme and provide them with opportunity to demonstrate their essential parts and new innovative technologies on orbit.

Features1. Low-cost and Short-term development

In the development of RAISE-3, MBSE (Model Based Systems Engineering) is attempted to improve the efficiency of satellite
development through digital development.
MBSE is partially applied to environment construction, system modeling, design, traceability and review.

Innovative Satellite Technology Demonstration-3 | 04

Innovative Satellites

2. Development by MBSE

CubeSat“Innovative Satellite Technology Demonstration Program” provides demonstration opportunities about once every two years,
and the RAISE satellite is required to be developed in less than two years and at a low cost. On the other hand, the RAISE
satellite needs to be reliable enough to acquire demonstration data from each device. Achieving both short-term, low-costdevelopment and ensuring reliability are important development issues for the RAISE satellite.
To challenge this development,- RAISE-3 consists of almost flight-proven components and little modified components from flight-proven components to shorten
the design and verification period, reduce development costs, and development risks.
- On-Board Computer (OBC) of RAISE-3, which is the key to satellite system control, has many small satellite heritages. This
OBC is equipped with a highly radiation-resistant CPU, ensuring high reliability.

Innovative Satellite Technology Demonstration Program

Satellite Systems

Innovative Satellite Technology Demonstration-3

Integrated Satellite Control System
The Integrated Satellite Control (ICS) subsystem has the core functions of the satellite system such as data handling oftelemetry commands, satellite management, and mission data processing. These ICS functions are provided by the
On-Board Computer (OBC). RAISE-3 OBC is based on the flight-proven OBC and ensures reliabilit y withmain/slave-redundant configuration.
Communication System

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

The communication subsystem consists of S-band and X-band. S-band is telemetry command lines for satellite control, andX-band is a telemetry downlink line that transmits experiment data of each theme, etc. from the satellite to the ground system.
The S-band communication components are flight-proven with a redundant configuration to improve reliability.
The X-band has sufficient downlink data rate to transmit the experiment data of all themes stored in the satellite system to theground system.
Electrical Power System
The Electrical Power Subsystem generates, stores, and supplies the power required for demonstration theme components,
satellite bus system components, and heaters.
On RAISE-3, solar panels are attached to the four sides of the satellite, and in the sunlight, one or more solar panels
continues to generate power enough to each experiment. Li-ion battery with high volumetric and mass efficiency is used tostore electric power.

Microsatellite

Attitude Control System
The Attitude Control Subsystem (ACS) controls the satellite attitude with the three-axis attitude control. ACS has an attitudechange maneuver function which enables attitude control necessary for satellite operation and experiments of eachdemonstration theme.
If the ACS component fails partially, the remaining components enable to continue attitude control. That improves therobustness of the satellite system.

RAISE-3 Configuration
CubeSatInnovative Satellites

05 | Innovative Satellite Technology Demonstration-3

Innovative Satellite Technology Demonstration Program

Main Characteristics
Epsilon Launch Vehicle

Launch Site

Uchinoura Space Center

Launch Year

JFY 2022

Innovative Satellite Technology Demonstration-3

LaunchLaunch Vehicle

Sun-synchronous orbit
560km

Inclination

97.6 degree

Local Sun Time at Descending Node

9 :30

Box-shape with body mounted solar array panels
Dimensions

1m × 0.8m × 1m ( Payload Adapter Fitting not included )Weight110 kgAttitude Control

Three-axis control ( Earth-pointing, Sun-pointing, etc. )Mission Term

Solar Array

Average during sunlight BOL : > 250 W, EOL : > 230 W

Mission system

BOL : max105Wh, EOL : max62 Wh

Microsatellite

Power(RAISE-3)

Shape

AltitudeRApid Innovative payload demonstration SatellitE-3

Orbit

Initial Operation 1month and Nominal Operation 13 months

CubeSatInnovative Satellites

Innovative Satellite Technology Demonstration-3 | 06

Innovative Satellite Technology Demonstration Program

Configuration

Innovative Satellite Technology Demonstration-3

RAISE-3

Dimensions 1m × 0.8m × 1m ( Payload Adapter Fitting not included )Weight 110kg

03 GEMINI

01 LEOMI

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

cots GPU based Edge-computing
for mission systems utilizing model
based systems engineering

Low Earth Orbit satellite MIMO
for 920MHz band IoT platform

04 KIR
Kakushin-3 water Ion-thruster
and Resistojet-thruster

05 TMU-PPTTokyo Metropolitan University
Pulsed-Plasma Thruster
Microsatellite

06 D-SAIL
Membrane deployment deorbit mechanism

02 SDRX
Software Defined Receiver

CubeSatInnovative Satellites

07 HELIOS
Harvesting Energy with Lightweight Integrated
Origami Structure
07 | Innovative Satellite Technology Demonstration-3

Innovative Satellite Technology Demonstration Program

Theme ofon-orbit demonstration

Theme name

On-orbit demonstration of 920 MHz band IoT platform that uses
satellite MIMO technology

Proposing organization

To demonstrate a satellite MIMO technology to improve thespectral efficiency of satellite links. In addition, this project
demonstrates a satellite IoT platform concept realizing ultra-widearea and protocol-free IoT services as a use case for expanding
the high-capacity downlink channel by MIMO technology.

LEOMI-TRX：150mm×150mm×150mm
LEOMI-LANT：172mm×172mm×42mm
LEOMI-XANT：71mm×71mm×22mm

Person responsible for
implementation

02
Theme name

JAXA

Software Defined Receiver “SDRX”
Software-defined radio that enables flexible satellite
development

Outline of mission

NEC Space Technologies, Ltd.

Demonstrate a method for developing sophisticated andcomplex satellite systems in a short time and at low cost, as
well as on-board rewrite/dynamic reconfiguration
techniques in orbit, utilizing digital data related to thedesign and related processes.
Weight©NEC Space Technologies, Ltd.

Innovative Satellites

150mm×150mm×150mm

Person responsible for
implementation

CubeSat

Proposing organization

Dimensions

Fumihiro Yamashita
Nippon Telegraph and Telephone Corporation
Microsatellite

Collaborators

Weight Set：4.0kg(RAISE-3)© Nippon Telegraph and Telephone Corporation

Nippon Telegraph and Telephone Corporation

RApid Innovative payload demonstration SatellitE-3

Outline of mission

Dimensions

Innovative Satellite Technology Demonstration-301

Low Earth Orbit satellite MIMO for
920MHz band IoT platform “LEOMI”

1.4kg

Masaharu Tsuchiya
NEC Space Technologies, Ltd.

Innovative Satellite Technology Demonstration-3 | 08

Innovative Satellite Technology Demonstration Program03

cots GPU based Edge-computing for mission systems
utilizing model based systems engineering “GEMINI”

Theme name

On-orbit evaluation and model-based development of a commercial GPU

Proposing organization

Mitsubishi Electric Corporation

Innovative Satellite Technology Demonstration-3

Outline of mission

O n - o r b i t d e m o n s t ra t i o n o f a c o n s u m e r G P U c a p a b l e o fultra-high-speed computation to enable high-speed signal processing
such as AI processing and SAR regeneration processing. In addition,
the software development for the GPU will be model-based, aiming
to shorten the development period and improve quality.

Dimensions

143mm×143mm×45mm© Mitsubishi Electric Corporation

Person responsible for implementation

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

04
Theme nameShinya Hirakuri

0.7kg

Mitsubishi Electric Corporation

Kakushin-3 water Ion-thruster andResistojet-thruster “KIR”
On-orbit demonstration of an ultra-compact integrated propulsion
system that uses water as a propellant

Proposing organization
Outline of mission

Microsatellite

Dimensions

WeightPale Blue Inc.

Aim to enhance competitiveness through on-orbit demonstrationof an ultra-compact integrated propulsion system that integrates
two types of propulsion systems, resist jet thrusters and ion
thrusters using water as the propellant, into a single component.
Weight 1.8kg

123mm×123mm×90mm

Person responsible for implementation

Jun Asakawa

05
CubeSatOn-orbit demonstration and performance evaluation of a pulsed plasma
thruster (PPT) for small satellites

Proposing organization
Outline of mission

Innovative Satellites

Dimensions

Pale Blue Inc.

Tokyo Metropolitan University
Pulsed-Plasma Thruster “TMU-PPT”

Theme name

Advanced Technology Institute, LLC

To conduct an on-orbit demonstration and performance evaluation ofan electric propulsion system that is low-power, compact, and low-cost
as a propulsion system for nano-satellites and small satellites.

160mm×130mm×100mm

Person responsible for implementation
Collaborators

09 | Innovative Satellite Technology Demonstration-3©Pale Blue Inc.

Weight 1.4kg
Mitsuteru Sugiki

Advanced Technology Institute, LLC

Tokyo Metropolitan University, University of Yamanashi,
Takahashi Denki Seisakusho Corp

06

Membrane deployment deorbit
mechanism “D-SAIL”

Theme name

On-orbit demonstration of membrane
deployment deorbit mechanism for microsatellites

Proposing organization

To further reduce the period of time that thesatellite remains in orbit after the end ofoperations, the system of deorbit
mechanisms will be validated.

2249mm×2080mm×73mm ( when deployed )1.9kg

Collaborators©Axelspace Corporation

Tomohiro Kawamura
Axelspace Corporation(RAISE-3)

Person responsible for
implementation

SAKASE ADTECH CO., LTD.

Theme name

Demonstration of a lightweight, membrane deployment
structure with power generation and antenna functionsfor Society 5.0

Proposing organization
Outline of mission

In order to achieve high performance (high power/ high capacit y 5G communication / highresolution obser vation by interferometr y) of
low-cost small satellites, on-orbit demonstration ofa lightweight, high-delivery membrane structurewith power generation and antenna functions will
be performed.

electric box：130mm×110mm×110mm
membrane structure (when deployed)：
1000mm×1000mm×230mm
Set：2.3kg

Person responsible for
implementation

Yoshiharu Sakai
SAKASE ADTECH CO., LTD.

Innovative Satellite Technology Demonstration-3 | 10

Innovative Satellites

WeightSAKASE ADTECH CO., LTD.

CubeSatDimensions©SAKASE ADTECH CO., LTD.

Microsatellite

07

Harvesting Energy with Lightweight Integrated
Origami Structure “HELIOS”

RApid Innovative payload demonstration SatellitE-3

WeightAxelspace Corporation
Innovative Satellite Technology Demonstration-3

Outline of mission

Dimensions

Innovative Satellite Technology Demonstration Program

Theme ofon-orbit demonstration

Innovative Satellite Technology Demonstration Program

Equipment that increases added
value of mission

Innovative Satellite Technology Demonstration-3

RAISE-3 is equipped with a component that increase added value of the mission.

01
OutlineOn Board Computer slice

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

The OBC slice is integrated into the SDR X to generate a
pseudo-modulated signal for evaluation of the software receiving part (Rxpart). A high-performance, small and low-power SOI-SOC MPU is used
to generate the pseudo-modulated signal. The MPU is being developed
for space applications and its radiation tolerance and operating system(OS) will be evaluated using OBC slice. As radiation tolerance evaluationof the MPU, on-orbit data acquisition of radiation tolerance of the MPU
internal memory and on-orbit evaluation of various IO and serial interfaceof the MPU are performed.

Dimensions

60mm×133mm×107mm

Development oraganization

Weight0.45kg(connection cable not included)

JAXA, Mitsubishi Heavy Industries, Ltd.
SOI-SOC MPU

Microsatellite
CubeSatOperation
Each demonstration theme proposer makes an experiment request to the ground system via a web browser. In the ground system,
based on the experiment request input and the experiment plan, satellite operation plan is created, and stored-command plan isgenerated.
The generated stored commands are uploaded to the satellite from the ground station, and the satellite conducts experiments oneach demonstration theme according to the stored commands and accumulates the experimental data in the onboard data
recorder.

Innovative Satellites

Accumulated experimental data is transmitted from the satellite to the ground system using the X-band telemetry downlink line. The
ground system sorts the acquired telemetry data for each demonstration theme, and then generates and stores them as data thatcan be distributed together with the satellite House Keeping data required for experimental data evaluation. The demonstration
theme proposer acquires experimental data via a web browser.
As described above, the demonstration theme proposer can obtain the convenience of being able to input the experiment request
and acquire the experiment data all via the WEB browser.
11 | Innovative Satellite Technology Demonstration-3

Innovative Satellite Technology Demonstration Program

RAISE-3 System Overview

Innovative Satellite Technology Demonstration-3

RAISE-3 Total System
Satellite System
PayloadGround System

S-bandCommandSatellite
controlS-bandX-bandDataprocessing /storing

Experiment request/
Experiment plan

planning

Demonstration
Theme Proposer

Experiment Data

distribution(RAISE-3)

S-bandTelemetry

Satellite
Control System

RApid Innovative payload demonstration SatellitE-3

X-bandTelemetry

GroundStation

Epsilon Launch Vehicle
Microsatellite

RAISE-3 Flight Model

CubeSatInnovative Satellites

Innovative Satellite Technology Demonstration-3 | 12

Innovative Satellite Technology Demonstration Program[ Theme of on-orbit demonstration ]Microsatellite
Launch vehicle is under adjusting

Innovative Satellite Technology Demonstration-3

01
Theme name

KOYOH
Development of a micro-satellite system for space scienceand engineering, and X-ray observation of gravitational
wave sources

Proposing organization
RApid Innovative payload demonstration SatellitE-3(RAISE-3)

Outline of mission

Dimensions

Kanazawa University

The satellite, KOYOH, has a wide field X-ray monitor,
and will identify the time and direction of gamma-ray
bursts and X-ray transient phenomena associated withgravitational wave radiation. It will share the observed
information to ground/space observatories in wholeover the world within quasi-real time.

493mm×450mm×488mm

Person responsible for implementation

Weight43kg

Satoshi Yagitani
Kanazawa University

Microsatellite

02

Platform for Extra and Terrestrial Remote
Examination with LCTF “PETREL”

Theme name

Demonstration of multi-spectral ocean observation technologythat uses an ultra-low cost high-accuracy attitude control bus system

Proposing organization
CubeSatOutline of mission

Innovative Satellites

Dimensions

Tokyo Institute of Technology

An innovative multispectral camera will be mounted on a low-cost but
high-performance microsatellite. This project including mission
operation and providing data application services is conducted by aquite unique academic-industrial consortium in which members
contribute via their own professionalities free of charge. This projectwill open up a new space business utilizing spectral data, and a
new research style of space science.

467mm×530mm×512mm

Person responsible for implementation
Collaborators

13 | Innovative Satellite Technology Demonstration-3

Team Umitsubame

WeightYoichi Yatsu

62kg

Tokyo Institute of Technology

Theme name

Demonstration of space tether technology for debris capture

Proposing organization

Dimensions

Shizuoka University
Innovative Satellite Technology Demonstration-3

Outline of mission

Innovative Satellite Technology Demonstration Program

03

Space Tethered Autonomous Robotic
Satellite “STARS-X”

A tether is extended 1km in space, and a robot(climber) moves on the tether to conduct a debris
capture experiment with a net.

540mm×588mm×576mm

Person responsible for implementation

Weight60kg

Interview People involved in “Innovative Satellite Technology Demonstration-3”

Microsatellite

Interview articles with each organization are on
the following website.

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

Masahiro Nohmi
Shizuoka University( Japanese only )CubeSat©Nagoya University©SAKASE ADTECH CO., LTD.

©Advanced Technology Institute, LLC©Kanazawa University

Innovative Satellites©Waseda University

Innovative Satellite Technology Demonstration-3 | 14

Innovative Satellite Technology Demonstration Program[ Theme of on-orbit demonstration ]CubeSatTo be launched by Epsilon Launch Vehicle No.6

Innovative Satellite Technology Demonstration-301

MAGnetically separating
NAno-satellite with Rotation for
Orbit control “MAGNARO”

Theme nameRotation and separation of microsatellites to deploy
their constellation

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

Proposing organization
Outline of mission

Dimensions

Nagoya University

We aim to establish a method to achieve resourcesaving, high accuracy, and formation by rotating
and separating connected nano-satellites to form aformation, and to achieve multi-point simultaneous
observation and continuous earth observation with
nano-satellites.

111mm×111mm×340mm

Person responsible for implementation

Weight4.4kg

Microsatellite

Takaya Inamori
Nagoya University

02

MITSUBA

Theme nameCubeSatOn-orbit demonstration aimed at expanding space application ofcommercial semiconductor devices and general-purpose equipment

Proposing organization
Outline of mission

Innovative Satellites

Dimensions

Kyushu Institute of Technology

On-orbit degradation observation of COTS semi conductor for
adding value to COTS data base and On orbit demonstrationof general USB device.

105mm×100mm×227mm

Person responsible for implementation

15 | Innovative Satellite Technology Demonstration-3

Weight1.7kg

Hirokazu Masui
Kyushu Institute of Technology

Theme name

KOSEN-2
Demonstration of technology for a marine observation data collection satellite equipped with a directional antenna
with ultra-high precision attitude control; Sustainable space engineer development; and Demonstration of a
network-based satellite development scheme

Proposing organization

National Institute of Technology (KOSEN), Yonago College

The project will collect observation data of seafloor crustal deformation by
combining a LPWA (LoRa) receiver and a directional antenna, demonstrate thehigh-precision attitude control using a dual reaction wheel that integrates fish-eye
cameras and magnetic sensors, and demonstrate satellite communications using
a satellite data collection protocol specialized for multi-point reception.

Dimensions

111mm×111mm×227mm

Person responsible for
implementation

2.7kg

Masahiro Tokumitsu
National Institute of Technology (KOSEN), Yonago College

National Institute of Technology (KOSEN), Gunma College

04

WASEDA-SAT-ZERO

Theme name

Demonstration of integral molding technology for satellite housing

Proposing organization

Waseda University

Aiming for zero screws, zero mechanical parts, and zero debris byusing 3D printer technology to mold the satellite chassis in one piece.
Using this satellite chassis, we will conduct deployment experimentsof a membrane surface composed of flat elements (like origami).

Dimensions

113mm×113mm×113mm

Person responsible for implementation

Theme nameTomoyuki Miyashita
Waseda University

FSI-SAT
Demonstration of technology for a multi-spectral camera for CubeSat

Proposing organization
Outline of
mission

1.2kg

CubeSat05

WeightMicrosatellite

Outline of
mission

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

Collaborators

WeightInnovative Satellite Technology Demonstration-3

Outline of
missionInnovative Satellite Technology Demonstration Program

03

Future Science InstituteA 1U size multispectral camera including data processing system will
be developed at low cost to demonstrate basic operation in orbit.

Person responsible for implementation

WeightInnovative Satellites

Dimensions 110mm×110mm×113mm

1.4kg

Mitsuharu Shiwa

Future Science InstituteInnovative Satellite Technology Demonstration-3 | 16

Innovative Satellite Technology Demonstration Program

Innovative Satellites

Innovative Satellite Technology Demonstration-3

Innovative Satellite Technology Demonstration-1

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

RApid Innovative payload
demonstration Satellite-1
RAPIS-1
JAXA

MicroDragon
Keio University

Rapid International ScientificExperiment Satellite
RISESAT
Tohoku University

Man-made meteor shower
Demonstration Satellite
ALE-1
ALE Co. Ltd.

Innovative Satellite Technology Demonstration-2

Microsatellite

RApid Innovative payload
demonstration SatellitE-2
RAISE-2
JAXA

Variable Shape Attitude Control
Demonstration Microsatellite
HIBARITokyo institute of Technology

The multi wavelength infraredobservation microsatellite
Z-Sat
Mitsubishi Heavy Industries, Ltd.

Debris Removal Unprecedented
Micro-Satellite
DRUMS
Kawasaki Heavy Industries, Ltd.

Innovative Satellite Technology Demonstration-3
CubeSatInnovative Satellites

RApid Innovative payload
demonstration SatellitE-3
RAISE-3
JAXA

KOYOH
Kanazawa University

Platform for Extra and Terrestrial
Remote Examination with LCTFPETRELTokyo Institute of Technology

Innovative Satellite Technology Demonstration-4

17 | Innovative Satellite Technology Demonstration-3

Space Tethered Autonomous
Robotic Satellite
STARS-X
Shizuoka University

Coming soon!

MAGnetically separating NAno-satellitewith Rotation for Orbit control
MAGNARO
Nagoya University

Innovative Satellite Technology Demonstration Program
Innovative Satellite Technology Demonstration-3

Advanced Satellite Toward
Exploration of dust enviRonment
with In-Situ Cosmic dust sensor
ASTERISC
Chiba Institute of Technology

Radio Amateur Satellite
NEXUS
Nihon University

Microsatellite

TeikyoSat-4
Teikyo University

Lunar Exploration Technology
Demonstration Satellite
Aoba VELOX-IV
Kyushu Institute of Technology

RApid Innovative payload demonstration SatellitE-3(RAISE-3)

Multi-Functional Deployable
Membrane Structure Demonstrator
OrigamiSat-1
Tokyo Institute of Technology

AGU Remote Innovative
CubeSat Alert System
ARICA
Aoyama Gakuin University

Advanced OBC of
NanoDragon
Meisei Electric Co. Ltd.

CubeSat for Technology Demonstrationof Jupiter Radio Observation
KOSEN-1
National Institute of Technology,
Kochi College

CubeSat

MITSUBA
Kyushu Institute of Technology

KOSEN-2
National Institute of Technology, Yonago College

WASEDA-SAT-ZERO
Waseda University

FSI-SAT
Future Science InstituteInnovative Satellites

Innovative Satellite Technology Demonstration-3 | 18