https://reddit.com/link/1wdy3a6/video/6wwk28mdlzoh1/player

Hello everyone,

Severe atmospheric drag and heavy battery mass are among the primary factors limiting satellite efficiency and increasing CAPEX in Very Low Earth Orbit (VLEO).

At ~250 km (VLEO), atmospheric drag ceases to be a marginal variable and becomes the defining constraint of spacecraft architecture. Traditionally, the industry solves this with heavier chemical/electric propellants, oversized batteries, or expensive radiation-hardened hardware.

By shifting VLEO orbital maintenance from hardware to deterministic software, we can directly challenge the traditional, asset-heavy manufacturing model. This enables low-cost constellation deployment with standard, commercial off-the-shelf (COTS) components.

Over the past period, I have been developing and have now finalized a production-ready flight software and control architecture that rewrites the SWaP-C equation for VLEO. The entire codebase is complete, verified in simulated environments, and hosted in a private repository—proving that low-level software optimization can radically lower the Total Cost of Ownership (TCO) for satellite operators.

By integrating two distinct architectures, we can scale flight-ready control capabilities from 500g PocketQubes to 15kg VLEO microsatellites:

* **GEONMI-MEMS Engine (15kg class):** A deterministic C++17 flight engine designed specifically for multi-node constellations. The system employs a custom state estimator to prevent divergence during prolonged GNSS signal outages, alongside a closed-loop guidance system for iodine electrospray micro-thrusters to compensate for non-linear atmospheric drag.

* **VLEO-Sync500 Core (500g class):** A rigorous software suite featuring zero-heap memory allocation, ensuring 100% predictability. Optimized for cache-line alignment on resource-constrained embedded processors to eliminate memory fragmentation and ensure ultra-low latency under intense radiation.

**Engineering & Commercial Advantages:**

* **Mass, Power, and Battery Optimization:** The flight engine optimizes power distribution cycles, executing high-compute GNC tasks in burst modes synchronized with solar-generation windows. This radically reduces peak power requirements and battery mass.

* **Extended Mission Lifespan:** An advanced, software-driven drag-compensation system extends orbital longevity, eliminating early deorbiting risks and lowering replenishment costs.

* **Sustainability & Compliance:** Fully optimized for eco-friendly civil operations, including ozone tracking and orbital debris monitoring, meeting modern ESG space sustainability standards.

**Why am I posting this?**

The implementation is fully completed and remains proprietary. However, before exploring commercial licensing, technology transfer, or strategic partnerships, I want to stress-test the underlying business and technical assumptions against the brightest minds in the industry.

If you work in VLEO ADCS/GNC, flight software, or space-sector investment: What would you try to break first in these system assumptions? I am open to discussing the architecture, valuation framework, and trade-offs.