Tungsten Alloy Satellite Gyroscope Counterweight — tungsten-alloy-satellite-gyroscope-d01.jpg

Tungsten Alloy Satellite Gyroscope Counterweight

Non-magnetic W-Ni-Cu inertial core for satellite attitude and stabilization control units — permeability < 1.01, ISO G0.4 dynamic balancing, ±0.005 mm machining tolerance, 100% X-ray / ultrasonic NDT verified.

Materials: W-Ni-Cu (non-magnetic)
Features: Zero-deflection non-magnetic composition, sub-micron machining precision, high-vacuum liquid-phase sintering, defect-free internal matrix
Application: Satellite attitude control units, instrumentation stabilization modules, high-precision orbital gyroscopes.

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Specifications

Parameter	Value
Material Composition	W-Ni-Cu (Non-Magnetic)
Magnetic Permeability	< 1.01 (Zero Deflection)
Dynamic Balancing Grade	ISO G0.4 Precision
Sintering Technology	High-Vacuum Liquid Phase
Machining Tolerance	±0.005 mm

FAQ

Frequently Asked Questions

What materials and process are used for Tungsten Alloy Satellite Gyroscope Counterweight?

Tungsten Alloy Satellite Gyroscope Counterweight is made from W-Ni-Cu (non-magnetic) 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 Satellite Gyroscope Counterweight?

Typical specifications: Material Composition: W-Ni-Cu (Non-Magnetic); Magnetic Permeability: < 1.01 (Zero Deflection); Dynamic Balancing Grade: ISO G0.4 Precision. 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 Satellite Gyroscope 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.