Applications

Space: Metal Seals Applications

Description

Omniseal® metal face seals are used in space launch vehicle and satellite applications where failure is not an option. Designed to perform in cryogenic, ultra-high vacuum, and extreme pressure environments, they meet stringent requirements for very low leakage and mission-critical reliability. Examples:

  • Launch Vehicle Tanks
  • Launch Vehicle Valves
  • Launch Vehicle Propulsion System Feedlines
  • Launch Vehicle Turbopumps
  • Launch Vehicle Combustion Chambers
  • Satellite Tanks
  • Satellite Instrumentation

Metal Face Seals For Launch Vehicles

Metal Spring-Energized C-Seals For Satellites

Metal Seals Launch Vehicles
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More Information

Temperature:

Pressure:

Leakage Rates:
Seal Diameter:

Cross Sections:

Clamping Load:
Surface Finish:
Oxygen Cleaning:

From -269°C to +1000°C (-452°F to +1832°F); higher temperatures available on request
From ultra-high vacuum (UHV) to 6894 bar (100,000 psi)
To 1×10⁻¹² mbar·l/s (plated + spin polished)
Face—8 mm to 7000 mm (0.3" to 275.6")
Axial—8 mm to 400mm (0.3" to 15.7")
0.79 mm to 12.70 mm (0.031" to 0.500"); non-standard available on request
Up to 150 N/mm
Face: Ra 0.2 to 1.6 um; Axial: Ra 10 um
As required


Depending on the type of Metal Seal, the solution can be used for static and semi-dynamic face or axial sealing in extreme temperature, pressure, vacuum, and radiation environments.

Applications include:

  • Low to moderate load with high spring back (C-Seal, V-Seal, E-Seal)
  • Medium to high load with increased spring back and wider sealing surface (Spring-Energized C-Seal)
  • Ultra-high vacuum and cryogenic sealing (Aluminium Spring-Energized Seal, O-Ring)
  • Shaft and bore sealing in semi-dynamic, rotary, and reciprocating applications (Axial C-Seal, Lip Seal, Comma Seal)
  • Non-circular and shaped geometries (Shaped Seal, Machined Seal)
  • High spring back for large flange movement or thermal cycling (V-Seal, E-Seal)
  • High seating stress for rough surface finishes or soft flange materials (Spring-Energized C-Seal, Aluminium Spring-Energized Seal)
  • Long-term static sealing under radiation exposure (C-Seal, Spring-Energized C-Seal)
  • Standard fitting interfaces (Boss Seal for AS5202, E-Seal for AS1895)

Case Studies

Discover in depth information and practical application tips in these use cases

Tags: Space High pressure applications Aerospace Launch vehicles & Satellites Cryogenic Applications