Spacecraft name |
Waseda-SAT0 (Waseda-Sat-Zero) |
Form factor |
CubeSat |
Units or mass |
1U |
Status |
Launch failure |
Launched |
2022-10-12 |
NORAD ID |
Launch failure |
Deployer |
E-SSOD (Epsilon Small Satellite Orbital Deployer) [JAXA] |
Launcher |
Epsilon |
Entity name |
Waseda University |
Institution |
University |
Entity type |
Academic / Education |
Headquarters |
Japan |
Oneliner |
Educational mission with drag chute for deorbiting.
|
Description |
- Evaluation of satellite body which made by Integral molding in space environment.
- Evaluation of performance and functions of a test body in space environment.
- Establishment of base technology about the super lightweight space structure technology that is necessary for future supersized space structure.
- Encouraging the talent carrying the next generation by an activity student mainly participate in as a part of a research of university education.
- Offer the opportunity of satellite tracking and operation for ham operators and amateur astronomers, and contribute to improvement of satellite communication technic ( 1 )
Minimum success: Establish communication between satellite and earth station.
Full success:
- Measure strain and temperature of satellite body.
- Announce the command to turn on the LED mounted on the satellite to amateur radio stations which use that frequency band Provide a satellite operation experience.
- Receive messages from general amateur radio stations which use that frequency band. Save it to memory. Downlink the messages few times.
- Recruit the message and we uplink it from command station. Downlink the messages few times.
- Extend and unfold a contained drag chute.
- Let down the altitude of orbit by using drag chute which suffer air resistance.
|
Sources |
[1] [2] |
Photo sources |
[1] [2] |
Keywords |
De-orbit device |
On the same launch |
|
Last modified: 2024-05-29