CAGE: 25CH7 · UEI: J3B7R2FBHMA3 · NAICS: 541715, 541713, 541330, 325180, 335991, 541511, 541512Federal contracting information

Embedded systems.
Advanced materials.

Abrams Research Systems LLC is an independent research company founded and operated by Joshua M. Abrams. Its core project, Abrams Event Address (AEA), gives events a precise address in space and time, with potential applications in space systems, electronic warfare, autonomous uncrewed systems, and hypersonic flight. Abrams also synthesizes graphene through flash Joule heating and explores its use in strengthening materials, improving existing components, and developing custom equipment and systems.

TRL 4 HOST-VERIFIED BASELINE: Passing deterministic test vectors on x86_64 today across Space Systems, Electronic Warfare (EW), Autonomous Uncrewed Systems (UxS), and Hypersonic Telemetry. Actively seeking defense laboratories, primes, and test range partners for SBIR Phase I / Direct-to-Phase II, OTA prototyping (TRMC / S²MARTS via NSTXL, DIU, SpaceWERX), and Range CRADAs to advance to TRL 5/6 on target flight silicon (ARM Cortex-R/M, LEON4, RAD750).
AEA-STATE/1 Multi-Node Operational Telemetry & Assured PNT Simulation above Earth
SIMULATION REGISTRY // ORBITAL & EW CONTESTED CORRIDOR
CONTESTED SENSOR FAILURE: Signal loss, velocity dropout, and spoofed GNSS fixes causing trajectory divergence and navigation filter collapse.
AEA-STATE/1 CANONICAL TRACE: Continuous 136-byte state synchronization (24B Context + 80B Kinematics + 32B SHA-256 Seal) maintaining deterministic truth without heap memory.
STRUCT SIZE
136B PACKED WIRE
MEMORY MODEL
0 MALLOC (#![no_std])
TARGET RUNTIME
<512B STACK (C99)
TIME REFERENCE
BIPM TAI SCALE
INTEGRITY SEAL
FIPS 180-4 PASS

Operational Integration

Where AEA solves real mission constraints.

Coordinate, timing, and memory constraints across three aerospace scenarios.

01

Electronic Warfare (EW) Resilience & GPS-Denied Assured PNT

Continuous TAI Epoch+
Mission constraint

Adversary Electronic Warfare (EW) jamming and coordinate spoofing sever GNSS uplinks and inject malicious time steps. Civil UTC time contains irregular leap-second insertions that cause computer clocks to repeat or freeze seconds, introducing kilometers of navigational error during high-velocity flight and collapsing navigation Kalman filters.

AEA approach

Standardizes on strictly monotonic International Atomic Time (TAI / TT) governed by BIPM paired with 3D velocity vectors, SO(3) attitude quaternions, and a 32-byte SHA-256 integrity seal. Executes deterministic dead-reckoning during GNSS denial, preserves metrology-grade timing, and rejects spoofed packets or bit-flips before they corrupt the flight loop.

WIRE GUARANTEE // EW APNT CONTINUITY
TIME SCALE: BIPM TAI (Scale 0x01)
PRECISION: u64 Seconds + u32 Nanoseconds
LEAP STUTTER: ZERO (Mathematically Immune)
GRAVITY W₀: Scalar Potential Calibration
02

Autonomous Weapons & Heterogeneous Swarm State Sync (UxS / CCA)

Zero Heap · Bitwise Parity+
Mission constraint

Collaborative Combat Aircraft (CCA) and attritable drone swarms (AUTOWARCOM / DRPM-UxS) combine mixed microcontrollers (ARM Cortex-R, LEON4, RISC-V, x86_64). Discrepancies in compiler struct padding, endianness, or floating-point negative zero (-0.0) create divergence in decentralized target state estimation.

AEA approach

Enforces a strictly packed 136-byte binary wire layout with normalized IEEE-754 floats (+0.0 canonicalization) and fixed Little-Endian byte ordering. Swarm nodes communicate peer-to-peer with exact bitwise parity across disparate architectures, enabling deterministic target handovers and decentralized consensus.

WIRE GUARANTEE // UXS STATE CONTRACT
STRUCT SIZE: 136 Bytes Fixed Wire
FLOAT NORM: Canonical +0.0 (IEEE-754)
ALLOCATION: 0 Malloc (<512B Stack)
SEU DETECT: FIPS 180-4 SHA-256 Seal
03

Hypersonic Plasma Blackout & Super Range Instrumentation

Truth-State Telemetry+
Mission constraint

Hypersonic vehicles (Mach 5+) experience thermal ionization plasma sheaths that sever RF uplinks, while disparate test range sensors (ground radar, optical mounts, telemetry pods) log in divergent coordinate frames, introducing multi-kilometer tracking uncertainty.

AEA approach

Runs within 0-malloc flight ring buffers to locally seal monotonic TAI truth states during blackout. Unifies range tracking radar (ITRF2020), hypersonic test articles, and orbital sensors (GCRS/BCRS) onto a single standardized 136-byte truth timeline for MACH-TB and Super Range corridors.

WIRE GUARANTEE // TRUTH TELEMETRY
BODY ORIGIN: NAIF ID 399 (Earth Geocenter)
FRAME ENUM: ITRF2020 (0x01) → GCRS (0x02)
PROPULSION: GNC Determinism Saves Δv Fuel
BLACKOUT LOG: Ring-Buffer Persistent Seal
Explore all 5 operational aerospace scenarios & wire transitions

Advanced Materials / RawCarbon

Graphene through flash Joule heating.

We synthesize non-Bernal turbostratic graphene through millisecond flash Joule heating (>3,000 K) without acid oxidation. Our applied research explores strengthening structural composites, improving existing components, and developing custom high-energy transformation equipment.

Explore Materials R&D

Institutional Teaming & Due Diligence

Federal vendor registration & technical evaluations.

INFO

Entity Identifiers & Classifications

Active SAM.gov+
Legal Entity
Abrams Research Systems LLC
Loveland, Colorado, USA
CAGE Code
25CH7
Active Commercial & Govt Entity
Unique Entity ID (UEI)
J3B7R2FBHMA3
SAM.gov Registered Vendor
NAICS Classifications (7 Approved)
541715, 541713, 541330, 325180, 335991, 541511, 541512
Physical Sciences R&D, Nanotech, Engineering, Graphite, Computing
EVAL

Structured Evaluation & Defense Teaming Protocol (TRL 4 → 5/6)

Air-Gapped Vault · OTA / CRADA+

We provide prime defense contractors and federal program offices with the zero-heap #![no_std] Rust static library, ANSI C header (include/aea.h), and offline test harness to measure worst-case execution time (WCET) and stack high-water marks on target flight silicon.

Behind the open-standard C-ABI interface, Abrams Research Systems LLC maintains an air-gapped R&D repository containing deep operational architectures for Autonomous Weapons (AUTOWARCOM / DRPM-UxS), EW Assured PNT, and Super Range instrumentation. Available for scoped evaluation under SBIR Phase I, Direct-to-Phase II (D2P2), OTA Prototyping (TRMC / S²MARTS, DIU, SpaceWERX), or Test Range CRADA.

Joshua M. Abrams, founder of Abrams Research Systems LLC

First-Principles Systems Engineering

Joshua M. Abrams

Founder & Principal Investigator, Abrams Research Systems LLC

contact@abramsresearch.net Federal contracting statement CAGE: 25CH7 · UEI: J3B7R2FBHMA3 · NAICS: 541715, 541713, 541330, 325180, 335991, 541511, 541512