Announced details
Applicable range of the high-G nonlinear rubber isolator: -40°C to 110°C. Applicable range of the cryogenic wire isolator: -170°C to 110°C.
Proposal and selection for a technology development topic under JAXA's Space Strategy Fund program. Capital and personnel relationships are Not disclosed.
National Research and Development Agency Japan Aerospace Exploration Agency. Other details are Not disclosed.
Trademark Registration No. 6956327. The expiration date is Not disclosed.
In this announcement the company addresses none of Contract Value / Offering price / Impact on Business Performance.
| Item | Details |
|---|---|
| Names of Products / Services Covered | Vibration damping mechanism usable across a wide temperature range, High-G nonlinear rubber isolator, Cryogenic wire isolator, Space Silicone Rubber® |
| Counterparty | National Research and Development Agency, Japan Aerospace Exploration Agency (JAXA) |
| Counterparty overview | National Research and Development Agency Japan Aerospace Exploration Agency. Other details are Not disclosed. |
| Relationship with the Company | Proposal and selection for a technology development topic under JAXA's Space Strategy Fund program. Capital and personnel relationships are Not disclosed. |
| Applicable area | Rockets, Artificial satellites, Satellites, Lunar exploration missions, Spacecraft exteriors, Lunar-surface operations |
| Registration number and expiry date | Trademark Registration No. 6956327. The expiration date is Not disclosed. |
| Quantitative Effects | Applicable range of the high-G nonlinear rubber isolator: -40°C to 110°C. Applicable range of the cryogenic wire isolator: -170°C to 110°C. |
Items this document does not state (11)
These are items the company does not state in this document. We do not leave them blank, nor fill them in from other sources or by inference.
The reasons the company gives
The company's own explanation, not something inferred from the numbers.To establish technology that protects onboard equipment from vibration and shock from launch through on-orbit and lunar-surface operations, and functions even in extremely low-temperature and high-radiation environments.