Load-bearing Structure of the Enclosure. Type 2
- Purpose: Mounting of spacecraft subsystem structure elements and equipment.
- Flight qualification of the product: Yes
- Brief history of flight qualification: Flight qualification since 2000.
- Possibility to adapt the product to customer requirements: Yes
Parameter | Value |
---|---|
Angle between intersection nodes of spiral fins , ° | 7.5° |
Angle between two spiralfins , ° | 42° |
Spiral fins thickness, mm | 10±1 |
Circumferential fins thickness, mm | 4±1 |
Longitudinal fins thickness, mm | 10±1 |
Distance between intersection nodes of spiral fins, mm | 396.25 |
Distance between circumferential fins, mm | 144.7 (251.5) |
High pressure metal-xenon tank unit | Yes |
Ring material (upper/lower) | CFRP on the basis of М55J / CFRP on the basis of М55J |
Cylindric grid shell made from CFRP with two interface rings.
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