IN JESUS I PRAY
IJIP 

 TECHNICAL DESCRIPTION

 

MANUFACTURER: APOKRISIS

FFL/SOT: 

LOCATION: HORN LAKE, MISSISSIPPI

 

I. Device Classification

• Type of Firearm: Silencer / Suppressor

• Model Designation: IN JESUS V1 IJIP

 

II. Physical Architecture & Construction Materials

• Chassis Geometry: Monolithic outer housing featuring an integrated multi-sided geometric profile, custom-engineered for additive manufacturing workflows using high-temperature polymer matrix composites (PAHT-CF) The complete configuration is documented in IN JESUS V1 IJIP (2).jpg.

• Coaxial Blast Core: Features a central linear bore path containing a fixed primary expansion chamber and an array of traditional internal acoustic baffle structures to catch, slow, and disrupt the primary gas frontier.

• Parallel Transpirational Channels: Positioned symmetrically and running parallel to the central bore axis are dedicated auxiliary cooling containment chambers. These parallel channels are structurally isolated from the straight flight path of the projectile but run adjacent to the primary baffle core.

• Side-Ported Vent Geometry: Precision-machined or printed lateral gas-routing ports link the internal baffle chambers directly to the parallel transpirational cooling channels, acting as pressure-gated bypass corridors.

• Internal Membrane Gating: The parallel cooling chambers are lined with independent micro-porous expanded Polytetrafluoroethylene (ePTFE) barrier membranes and protective structural wire mesh interfaces, capturing and sequestering a sacrificial, endothermic phase-change ablative media (ballistic gel compound).

 

III. Method of Operation & Signature Reduction Mechanics

The device attenuates muzzle blast and suppresses thermal/acoustic signatures via a multi-axis gas scavenging process:

1. Primary Capture and Deflection: Upon projectile discharge, high-pressure propellant gases travel down the coaxial bore line, entering the primary expansion chamber where initial pressure spikes are mechanically dispersed.

2. Side-Ported Scavenging: As pressure builds within the primary baffle core, a calculated volume of the superheated propellant gas is forced laterally outward through the side-ported vents, diverting gas energy away from the primary projectile path.

3. Parallel Transpirational Cooling: The diverted gases enter the parallel channels, forcibly interacting with the ePTFE barrier membranes and metal mesh interfaces. This high-pressure contact forces the sequestered ablative gel compound to undergo an instantaneous endothermic phase change (Latent Heat of Vaporization).

4. Thermodynamic Pressure Suppression: By instantly stripping substantial thermal energy away from the gas matrix within the parallel channels, the overall gas volume and pressure density are drastically minimized before the gas re-stabilizes or vents. The cooled, lower-velocity exhaust gas smoothly exits the forward face of the unit, mitigating the extreme thermal delta typically responsible for secondary muzzle flash and intense acoustic shockwaves.