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Designed for placing optoelectron devices, antenna
scanners, attitude control system transmitters and others on space communication
and navigation vehicles and scientific platforms.
The structures ensure a stable linear and angular position of devices and equipment under conditions of high vacuum and sign-variable cyclic thermal effects over a temperature range of -100°C to +100°C during all period of active space vehicle existence (at least 7 years). |
| Characteristic | Value |
| Integral coefficient of linear thermal expansion, degree -1,not more than | 0.15*10-6 |
| Specific strength, km, not less than | 110 |
| Specific elastic modulus, km, up to | 16000 |
For more details please contact us at:
| Adress: Khotkovo, Moscow region, 141371, Russia |
| Phone: (095) 584 - 55 - 11 |
| Fax: (09654) 3 - 13 - 13 |
| E-mail: tsniism@dataforce.net |
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