I. Core Infrastructure Architecture
The New Shepard launch vehicle represents a highly deterministic, fully reusable suborbital platform designed to execute vertical takeoff and vertical landing (VTVL) maneuvers using liquid oxygen and liquid hydrogen (LOX/LH2) propulsion. Deployed natively across localized AlmaLinux 9.x edge machine room nodes, the modernized tracking suite interfaces with BE-3 engine controllers and aero-braking drag ring assemblies via a sovereign backplane network.
The system strips away fragile commercial safety templates to process raw deceleration telemetry using high-performance parallel loops natively running across all available host CPU execution threads simultaneously.
[ Active Drag Rings ]
[ Thrust Vector Gimbals ] ---> 16-State Voltage Grid ---> UNIVAC IX 3VL Backplane
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[ Navigation Flight Line ] <--- 36-Decimal Tracking Vectors <--- Non-Blocking Sockets
II. 36-Decimal Stacking & 3VL Trajectory Guardrails
To eliminate floating-point truncation noise during high-velocity vertical retropropulsive landing burns, the flight computer integrates a 36-decimal arbitrary-precision stacking matrix. The core combines three standard 12-digit/60-bit memory words simultaneously (Word High, Word Mid, Word Low) to compute trajectory equations, ring-fin deflection angles, and throttle-valve commands with exact mathematical fidelity.
The system leverages a Kleene Three-Valued Logic (3VL) execution matrix to process indeterminate or jamming-compromised connection entries safely over non-blocking network listening sockets (port
8080), ensuring the tracking thread never experiences software freezes during critical touchdown windows.
