| Brand Name: | DLX |
| Model Number: | inconel 718 |
| MOQ: | 10kg |
| Payment Terms: | L/C,D/A,D/P,T/T,VTB |
| Supply Ability: | 1200 tons per month |
Engineered specifically for critical propulsion and high-pressure aerospace systems, our high yield strength Inconel 718 plate (available in hot rolled 5mm to 50mm thicknesses) delivers the uncompromising structural integrity required for rocket motor casings, liquid propellant thrust chambers, and severe-environment pressure containment. Manufactured through advanced double-vacuum melting processes (VIM + VAR) and controlled thermomechanical processing, each high yield strength Inconel 718 plate exhibits isotropic mechanical reliability, exceptional fracture toughness, and superior resistance to post-weld strain-age cracking. With precision leveling and tight dimensional tolerances, this hot rolled 5mm to 50mm material provides aerospace engineers with unmatched reliability under extreme multi-axial stress fields.
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Modern rocket motor casings endure tremendous internal ignition pressures, severe mechanical vibration, and rapid temperature spikes. To prevent catastrophic wall failure, structural materials must maintain high strength without sacrificing ductility. Our high yield strength Inconel 718 plate is metallurgical engineered to overcome these challenges, outperforming conventional alloys under simultaneous mechanical and thermal loads.
The superior performance of our hot rolled Inconel 718 plate (5mm to 50mm) stems from controlled precipitation hardening. By balancing niobium additions with targeted thermal processing, the alloy forms microscopic gamma double prime (γ′′) precipitates that lock the crystalline matrix. This unique metallurgy provides our high yield strength Inconel 718 plate with outstanding resistance to strain-age cracking during the roll-bending, electron-beam welding, and final assembly of cylindrical and hemispherical rocket motor casings.
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| Element | Content Range (%) | Element | Content Range (%) |
|---|---|---|---|
| Nickel (Ni) + Cobalt (Co) | 50.00 – 55.00 | Molybdenum (Mo) | 2.80 – 3.30 |
| Chromium (Cr) | 17.00 – 21.00 | Titanium (Ti) | 0.65 – 1.15 |
| Niobium (Nb) + Tantalum (Ta) | 4.75 – 5.50 | Aluminum (Al) | 0.20 – 0.80 |
| Iron (Fe) | Balance (Rem.) | Cobalt (Co) | ≤1.00 |
| Carbon (C) | ≤0.08 | Silicon (Si) / Manganese (Mn) | ≤0.35 each |
| Phosphorus (P) / Sulfur (S) | ≤0.015 each | Boron (B) | ≤0.006 |
| Property | Ambient Temp (20∘C) | Elevated Temp (650∘C/1200∘F) | Cryogenic Temp (−196∘C) |
|---|---|---|---|
| 0.2% Yield Strength (Rp0.2) | ≥1030 MPa (150 ksi) | ≥860 MPa (125 ksi) | ≥1180 MPa (171 ksi) |
| Tensile Strength (Rm) | 1240−1450 MPa | ≥1000 MPa | ≥1550 MPa |
| Elongation at Break (A5) | ≥15% | ≥12% | ≥18% |
| Hardness (HRC) | 36−44 HRC | — | — |
| Density | 8.19−8.22 g/cm3 | — | — |
| Melting Range | 1260∘C−1336∘C | — | — |
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Product FAQ
Q1: Why choose high yield strength Inconel 718 plate for rocket motor casings?
A: Inconel 718 combines high yield strength (>= 1030 MPa), high stiffness, and oxidation resistance from -253°C to 650°C. It avoids the high-temperature strength loss of titanium and the propellant embrittlement of maraging steels.
Q2: What heat treatment states are available for 5mm to 50mm Inconel 718 plates?
A: We provide three standard delivery conditions:
Q3: How to weld hot rolled 5mm to 50mm Inconel 718 plates without cracking?
A: Niobium additions slow precipitation kinetics, minimizing strain-age cracking. Weld in the solution-annealed condition via TIG, Plasma, or Electron Beam (EBW) with matching nickel filler, followed by aging to restore parent-metal strength.
Q4: How are heavy Inconel 718 plates packaged for export?
A: Plates are surface-passivated, interleaved with moisture barriers, strapped with steel bands, and secured on fumigated wooden skids or in reinforced wooden crates to prevent surface damage and bending.
Q5: What are the MOQ and lead time for custom Inconel 718 plates?
A: We offer dynamic project-specific MOQs. In-stock plates ship immediately; custom-rolled thicknesses and cut-to-size blanks require 3 to 5 weeks.
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