Tungsten Alloy Aircraft Radar Equipment Counterweight
Non-magnetic W-Ni-Cu counterweight for airborne radar and radome assemblies — 17.0–17.8 g/cm³ of concentrated mass that shifts resonant frequency away from airframe vibration with zero magnetic interference.
- Materials
- W-Ni-Cu (non-magnetic option)
- Features
- Zero magnetic interference, high-efficiency vibration damping, compact low-profile integration, electro-nickel / zinc coatings
- Application
- Nose cone radomes, avionics bays, electronic warfare (EW) suites and sensitive phased-array radar installations.
Specifications
| Parameter | Value |
|---|---|
| Alloy System | W-Ni-Cu (Non-Magnetic Option) |
| Density | 17.0 – 17.8 g/cm³ |
| Vibration Damping | High Efficiency |
| Magnetic Interference | Zero (W-Ni-Cu) |
| Surface Coating | Electro-Nickel / Zinc |
Frequently Asked Questions
What materials and process are used for Tungsten Alloy Aircraft Radar Equipment Counterweight?
Tungsten Alloy Aircraft Radar Equipment Counterweight is made from W-Ni-Cu (non-magnetic option) and is formed by MIM/PM (metal injection molding / powder metallurgy) near-net-shape and sintered to a relative density of ≥ 98%, which keeps mechanical properties close to wrought material.
What are the key specifications of Tungsten Alloy Aircraft Radar Equipment Counterweight?
Typical specifications: Alloy System: W-Ni-Cu (Non-Magnetic Option); Density: 17.0 – 17.8 g/cm³; Vibration Damping: High Efficiency. The full parameter list is in the specifications table on this page; custom requirements can be discussed against your drawing.
What is the MOQ and lead time for Tungsten Alloy Aircraft Radar Equipment Counterweight?
MOQ is 1000 pcs. Mold lead time is about 20 days (mold fee typically RMB 20–40k depending on part geometry), and production lead time is about 7 days once the mold is validated; secondary processing adds 3–5 days.
Related Products
Tungsten Alloy Aerospace Turbine Counterweight
Materials: W-Ni-Fe heat-resistant heavy alloy
High-temperature creep resistance, ≥ 400 MPa yield @ 400°C, net-shape PM molding, passivation / electro-nickel options
View Details
Tungsten Alloy Aircraft Aileron Counterweight
Materials: W-Ni-Fe heavy alloy
Sintered density ≥ 17.5 g/cm³, high yield strength, superior impact toughness, electro-nickel / chrome plating / passivation options
View Details
Tungsten Alloy Aircraft Flap Counterweight
Materials: AMS-T-21014 Class 1 tungsten heavy alloy
AMS-T-21014 Class 1 certified, multi-axial hydraulic compaction, precision grooves and mounting slots, >500 h salt-spray plating
View Details
Tungsten Alloy Aircraft Rotor Balance Counterweight
Materials: W-Ni-Fe (AMS-T-21014)
Near-net-shape liquid-phase vacuum sintering, flawless batch uniformity, ≥ 16 J/cm² impact toughness, full batch traceability
View Details