Main performance of an Angular Velocity Sensor based on HRG (being developed):
|
|
|
Continuous operation time |
15 years |
General operation time |
20 years |
Random deviation of zero signal from standard |
0.05°/h |
Maximum rate |
± 10°/sec |
Angle noise 3 σ (per 10Hz) |
< 1” |
Power consumption (4 axis) |
6 W |
Temperature range |
-30 ÷ +80°С |
Readiness time |
< 30 sec |
Vibration resistance within 35-1000 Hz |
25 — 5000 g |
Volume |
2700 cm3 |
Weight |
3 kg |
with redundant electronics |
3.5 kg |
Probability of failure-free operation (15 years) |
0.775 |
with redundant electronics |
0.991 |
Free from electromagnetic and radiation interference |
|
|
|
|
|
|
Four identical measuring
channels of HRG in FTR mode |
Power unit |
Communication unit
(Manchester-2
+ technological RS-232) |
|
Space activity license № 884К dated 2008-02-26
“Manufacture of Angular Velocity Sensor based on HRG for Spacecrafts of Scientific Application”.
.