Products/AL-NH₃ Heat Pipes

Core Technology

AL-NH₃ Heat Pipes

Aluminum-ammonia heat pipes with 15,000 W/mK effective thermal conductivity — 37× solid copper. Three construction variants from proven groove wicks to fully 3D-printed geometries.

Space-Grade Design · 3D-Printed Wick · 15,000 W/mK
EW JET AL-NH₃ Heat Pipe
15,000W/mK
Effective conductivity
30W/cm²
Maximum heat flux
≤3m
Transfer distance
Zero
Leak risk
Request Datasheet

Technology

Proprietary 3D-Printed Wick

EW JET's sintered wick geometry is designed computationally — capillary radius and permeability are controlled parameters, not a consequence of tooling. Enables wick performance not achievable with machined grooves or standard sintered powder.

Aluminum-Ammonia Working Pair

NH₃ has high latent heat of vaporization and a wide liquid operating range. Chemically compatible with aluminum — no copper liner required. Well characterised across the full space thermal environment.

Space-Grade Design Process

Designed with reference to ESA/ECSS space engineering standards. Vibration, thermal-vacuum, and leak testing available per qualification plan. Contact us for testing protocol documentation.

Aluminum Extrusion Body

6000-series alloy extrusion body. Precise internal channel dimensions, low mass, compatible with standard spacecraft mounting interfaces. Leak-tested 100% of units — fully enclosed system.

Applications

GEO Satellites

Long-duration comms and broadcast payloads. 15+ year mission life with no active components or maintenance access.

LEO / SAR Satellites

Rapid thermal cycling under −100°C to +100°C orbit environment. High-flux SAR payloads where groove wicks reach their capillary limit.

CubeSat & SmallSat

Compact custom assemblies for 1U–3U platforms and 50–200 kg smallsats. 3D-printed body enables tight-fit structural integration.

Construction Variants

Three product types — different wick structures for different requirements. Choose based on heat load, tilt tolerance, and geometry constraints.

Groove Wick
Extrusion + Axial Groove
Production

Extruded aluminum body with machined axial grooves as the wick. The groove geometry is fixed by the extrusion die — no custom pore structure. Standard form factor used in spacecraft thermal control for decades.

Advantages

  • Shortest lead time — die-extrusion production
  • Lowest unit cost at volume
  • Extensive space flight heritage
  • Straightforward qualification path

Limitations

  • Lower Q_max than sintered/3D-printed wicks of same OD
  • Performance degrades significantly at adverse tilt
  • Not suitable for high-flux or vertical mounting

Choose this when

Your heat load is within the groove wick Q_max envelope, pipe is roughly horizontal, and cost or delivery schedule drives the decision.

3D Wick Insert
Extrusion + 3D-Printed Wick
Production

Standard extruded aluminum body with EW JET's proprietary 3D-printed sintered wick insert. The wick pore geometry is computationally optimised — much finer capillary structure than machined grooves, in the same pipe envelope.

Advantages

  • Higher Q_max vs groove wick at same OD
  • Handles adverse tilt — capillary pressure overcomes gravity head
  • Custom wick geometry per application
  • Proven extrusion body — existing spacecraft interfaces fit

Limitations

  • Higher cost than groove variant
  • Longer lead time — printed wick insert

Choose this when

Q_max requirement exceeds what groove wicks can deliver, or the heat pipe must operate at adverse tilt (evaporator above condenser).

Full 3D Printed
Additive Body + Integrated Wick
R&D

Entirely additive-manufactured aluminum — body and wick printed as a single integrated piece. The key capability is geometry freedom: non-circular cross-sections, L-bends, curved paths, and integrated mounting features that extrusion cannot produce.

Advantages

  • Arbitrary geometry — curved, branched, non-circular
  • Integrated mounting bosses and interface features
  • Novel wick topologies — gradient porosity, lattice structures
  • No straight-pipe constraint on structural layout

Limitations

  • R&D stage — performance not fully characterised
  • As-printed Al has lower thermal conductivity than wrought alloy
  • Longest lead time — custom per geometry
  • Higher cost

Choose this when

Spacecraft structure doesn't accommodate a straight round pipe — curved routing, flat panels, or tightly integrated thermal-structural design is required.

Side-by-Side Comparison

Groove Wick3D Wick InsertFull 3D Printed
Body constructionExtrusionExtrusionAdditive (SLM)
Wick typeAxial groove3D-printed insert3D-printed integral
Q_max (300 mm)TBD WTBD WTBD W (R&D)
Rth (300 mm)TBD K/WTBD K/WTBD K/W (R&D)
Adverse tiltTBD°TBD°TBD (R&D)
Custom geometryOD / length onlyWick pore geometryFull 3D freedom
Lead timeShortMediumCustom / R&D
Production statusReadyReadyOn request

Q_max and Rth values pending test data. All TBD values measured at 300 mm test length — see Performance Data below.

Specifications

Values marked TBD are variant- and configuration-dependent. Contact us for a scoped datasheet.

Effective thermal conductivity
15,000W/mK
37× solid copper
Maximum heat flux
30W/cm²
High-flux payload ready
Maximum heat transport
TBDW
Varies by variant and length
Heat transfer distance
≤3m
Capillary-driven
Thermal resistance
TBDK/W
Varies by variant and configuration
Working fluid
NH₃
Ammonia, space-grade
Body material
Al alloy
6000-series extrusion / additive
Operating temp range
TBD°C
Wide cryogenic to high-temp
Vacuum compatibility
Yes
Fully enclosed, zero outgassing
Orientation sensitivity
Variant
Groove: high · 3D insert: low
Leak testing
100%units
Every unit inspected
Design reference
ESA/ECSS
Space engineering standard

Full datasheet on request. All performance values vary between Groove Wick, 3D Wick Insert, and Full 3D Printed variants.

Performance Data

Test basis: 300 mm length, same outer diameter, NH₃ working fluid, horizontal orientation. Fixing length and OD isolates wick structure as the only variable.Note: Performance varies with pipe length — longer pipes have higher transport resistance and lower Q_max. Datasheet for your specific length available on request.

300 mm · OD: TBD · NH₃ · horizontal (0°)
Temperature (°C)
50 W300 W500 W1,000 W1,500 W
Data pending — contact us for preliminary results

Performance varies with pipe length, OD, and operating temperature. Longer pipes have lower Q_max due to increased transport resistance.

Request datasheet

Why Aluminum-Ammonia

Common alternatives each have a critical limitation that AL-NH₃ avoids.

vs. Copper / Water Pipes
  • Compatible with aluminum spacecraft structures — no galvanic corrosion risk
  • NH₃ works across cryogenic-to-high-temp range that water cannot cover
  • ~3× lower mass per metre vs copper body at equivalent transport capacity
vs. Pyrolytic Graphite Sheet (PGS)
  • 3D routing — not constrained to flat, thin sheets
  • Higher total heat transport (W), not just high in-plane conductivity
  • Robust to launch vibration and structural loads
vs. Loop Heat Pipes / CPLs
  • Simpler construction — no compensation chamber, reservoir, or grooved saddle
  • Lower unit cost for standard transport lengths
  • No startup or priming sensitivity

Custom Configuration

Tell us your heat load, available pipe envelope, operating temperature, and orbit or mounting orientation. We scope the right variant, OD, and length.

Start a Design Conversation

Questions about custom geometries or qualification? Talk to our engineering team.