Except the ignorance is entirely on your end. When I show documents that show testing with integral composite armor that has spall liners incorporated, you try to claim ‘IT’S ONLY ON VEHICLES THAT HAVEN’T BEEN PRODUCED’ when the document came to no such conclusion. They never limited the reach of the technology, they only mention a couple programs that incorporated it. You continue to claim to know about the Abrams armor despite it still being classified.
Then your buddy throws a fit because a spall liner between glass layers can’t possibly have a similar application or effect on metal…despite having linked studies demonstrating as much.
Between the documents talking about the XM1 having spall liners, analysts and historians speaking of spall lining in Abrams tanks, official Army DTIC documents explicitly mentioning spall liners in Abrams tanks…even these studies you can see for yourself that incorporate spall mitigation between metal layers…and you still make claims that have been disproven. XD
There is no helping clowns like you. But if you want to ignorant, here are the sources you refuse to acknowledge.:
https://www.sciencedirect.com/science/article/pii/S2214914723001186
’ Moreover, each sequence of the distinct materials, properties and mechanical impedance are significantly important for the performance of the whole structure. Consequently, each of the different laminate has an important role towards preventing projectile piercing of the armour. The two frontal laminates (face sheet and strike face) fragmentate and mitigate the projectile’s nose. The two rear laminates (intermediate and back plate) hold the frontal plates, stop their fragments and absorbs ∼40% of the projectile kinetic energy. Hence, the strike-face should have high hardness and compression strength to break the tip of the projectile and the face-sheet should contribute to the spall protection, from spalls created by the strike-face fragmentation, on the front of the armour and to hold the strike face in position after the impact of a projectile. The subsequent laminates (intermediate and backplate) should have high toughness and energy absorption, to absorb a significant amount of energy during the impact of the projectile, while the third laminate has a great tensile strength to hold the strike-face’s fragments and protect the contact between the strike-face and the backplate. The back plate of common composite protection system is usually made up of a high-density material, especially metals, thus contributing the most to the total mass of the armour system. This research focuses on the reduction of the mass of the backplate and overall composite armour system, through the utilisation of ultra-light weight materials as backplate. The proposed materials is a Metal Matrix Composite (MMC) reinforced by nanomaterials which is designed and manufactured with enhanced mechanical and ballistic properties.’
’ 2.2.2.1. First laminate: face-sheet
The first laminate (face-sheet) is used for the spall protection, after the projectile impact preventing the micro damage to the following strike-face, protection from possible damage associated with system vibrations, protection from various environmental factors (i.e., thermal stress, ultraviolet radiation) and low Radar Cross Section (RCS) signatures. The basic functional requirements for the face-sheet layer are high dynamic stiffness, high-speed inelastic resistance to deformation, high compressive strength, and desirable hardness. These requirements contribute towards the main function of the strike face which is the mitigation of the projectile’s nose and/or the fragmentation and high shear strength due to the shearing behaviour of the material.’
’ 2.2.2.4. Fourth laminate: backplate
The backplate (last laminate layer) is used to absorb the projectile’s remaining kinetic energy through the plastic deformation mechanism, provide structure support to all of the protection laminate, and act as a load bearing element during the post impact period after the damage have taken place in the strike-face, support the strike-face body post-impact fracturing, and deform during the impact and recovery stages producing a high bending recovery and reaction. The backplate basic functional requirements are high toughness (rupture), high flexural strength, high bending stiffness, high fracture strength, suitable thickness (thin plates fail in tension due to the lack of structural rigidity), in-plane and through-the-thickness ductility (since this layer should be in deformation correspondence with the intermediate plate) and support the intermediate layer to avoid surpassing its bending strength under the projectile impacting. The backplate is a very important laminate of the composite armour since it absorbs up to the 40% of the kinetic energy.
Ductile materials, such as metal and polymer fibre composites, are ideal for use in the backplates. Metals are the most common material used for backplate due to low brittleness compared to polymer fibre composites.’

lol. Spall liners before metal layers, metal layers are ideals for backplates. An internal spall liner works with glass layers, even though glass is very brittle and prone to spalling. These internal spall liners are used in ballistic glass. Something that catches projectiles, and still resists spalling BECAUSE of a spall liner BETWEEN the spalling surfaces.
Deny it all you want, you’re still wrong.