Projects
For details on the Innovative Satellite Technology Demonstration Program, please refer to the JAXA website:
RAPIS-1
Space innovation starts here
Mission Complete
RAPid Innovative payload demonstration Satellite 1 (RAPIS-1) is the first demonstration mission in Japan Aerospace Exploration Agency (JAXA)‘s Innovative Satellite Technology Demonstration Program. It is designed to carry new components developed by Japanese private companies, universities and research institutes, allowing them to demonstrate their capabilities in the actual space environment. Axelspace is responsible for the design, construction and in-orbit operation of the satellite.
| Demonstration Theme Title | Institution |
|---|---|
| Evaluation of space environment tolerance of an innovative FPGA on the orbit | NEC |
| 2-3 Gbps X-band downlink in-orbit demonstration | Keio University |
| Green Propellant Reaction Control System (GPRCS) in-orbit demonstration | Japan Space Systems |
| Space Particle Monitor (SPM) in-orbit demonstration | |
| Innovative deep learning attitude sensor/star tracker development | Tokyo Institute of Technology |
| Light-weight solar panel apparatus | JAXA |
| Miniaturized low-power GNSS receiver in-orbit demonstration | Chubu University |
| Dimensions | 1022 x 1082 x 1060mm |
|---|---|
| Mass | about 200kg about 35kg for payloads |
| Downlink rate | 10Mbps |
| Attitude control | Three-axis control (Earth-pointing, Sun-pointing, ground point tracking, despin modes) |
| Attitude stability | within 300arcsec (allowed time 0.2sec) |
| Bus power generation | about 100W |
| Payload power generation | about 100W |
| Payload power consumption | about 56W in average, max 130W |
The bus system of this satellite is designed for high independence between mission systems and bus systems. It is thus an optimal setup for experimental components and is easily adaptable for future enhancements in functionality.
| Launch Date and Time | January 18, 2019 9:50:20 AM (Japan Standard Time) |
|---|---|
| Launch Vehicle | Enhanced Epsilon rocket |
| Launch Base | Uchinoura Space Center, Japan |
| Orbit | Sun synchronous, 500±20km altitude |
Track record
Our projects
WNISAT-1
HODOYOSHI-1
WNISAT-1R
GRUS-1A
RAPIS-1
GRUS-1BCDE