Axial Grooved Heat Pipes
Flight-proven spacecraft heat pipes (450 W·m transfer, Ø6–20 mm, up to 6 m, -133 to +227 °C) with 100+ satellite heritage. Customizable.
Technical specifications
- Purpose
- Thermal control of spacecraft equipment
- Year of release
- 1996
- Guaranteed service life, years
- 25 (after filling with working fluid)
- Estimated production/delivery time
- 2 months
- Flight heritage
- Successfully operated on more than 100 Russian and foreign satellites
- Customization
- Can be adapted to customer requirements
- Maximum transferred heat power
- 450 W·m
- Outer diameter, mm
- 6–20
- Length
- Up to 3.5 m (up to 6 m by special order)
- Operation temperature range, °C
- -133 to +227
- Minimum pipe bending radius
- 5 × outer diameter
- Working fluids
- Toluene, Ammonia, Propylene, Ethane, Methane, Nitrogen
- Configuration
- Straight or bent
- Type
- Two-phase hermetic closed evaporating/condensing system
- TRL
- 9 (flight-proven)
About
The Axial Grooved Heat Pipes are two-phase (vapor/liquid) hermetic closed evaporating/condensing thermal transfer systems for spacecraft equipment thermal control. They transfer up to 450 W·m, have outer diameters of 6–20 mm, and lengths up to 3.5 m (or 6 m by special order). Working fluids include Toluene, Ammonia, Propylene, Ethane, Methane, or Nitrogen. Operating temperature range is -133 to +227 °C. Minimum bend radius is 5 × pipe outer diameter. Available in straight or bent configurations. Released in 1996, 25-year service life after filling with working fluid, 2-month delivery. Successfully operated on more than 100 Russian and foreign satellites.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
