SOLARIS ONE
SOLARIS ONE — Self‑Sustaining, Recallable Solar‑Powered Space Rocket
An advanced investor-grade concept: stays in orbit on solar power, navigates with AI, and returns via the shortest energy-optimal path when recalled.
Executive Summary
SOLARIS ONE is a solar-electric hybrid orbital rocket engineered for indefinite operation in space. It uses deployable ultra-thin solar wings, solid-state energy storage, and ion-electric propulsion to remain active in orbit for years. When a return is required, an AI-driven recall algorithm computes the shortest, safest, and most energy-efficient trajectory back to Earth.
Core Innovations
Power & Structure
- Foldable triple-layer perovskite + multi-junction solar wings
- Carbon-carbon composite body with re-entry thermal shield
- Solid-state batteries + supercapacitor buffer
Propulsion & Guidance
- Chemical engines for launch and landing
- Hall-effect / Xenon ion thrusters for sustained maneuvers
- AI orbital recall algorithm — shortest-path, minimum ΔV
Shortest‑Distance Recall System — How It Works
- AI maps current orbital state and Earth rotation.
- Computes candidate de‑orbit windows (including gravitational assists).
- Optimizes for minimum ΔV and thermal constraints.
- Performs ion‑thrust alignment and solar-charged de‑orbit burn.
- Executes autonomous atmospheric entry and powered landing.
Applications & Markets
Commercial and government markets include satellite servicing, orbital logistics, space tourism transfer, emergency astronaut extraction, and defense surveillance. The product fits both B2B contracting (leases, retrieval) and B2G (government) revenue models.
Pitch Deck Highlights (12 slides)
Title: SOLARIS ONE\nTagline: Powered by the Sun. Controlled by Intelligence.
Rockets are disposable and fuel-dependent; satellites often cannot be recovered; missions cost too much.
Solar-powered rocket that stays in orbit indefinitely and returns on demand via AI shortest-path.
Technical White Paper Summary
Highlights: 180 kW peak solar generation, solid-state battery bank, Hall-effect ion thrusters, AI recall algorithm, radiation-hardened systems, and a mission profile supporting 3–12 tons of cargo or an optional crew module (0–6).
| Parameter | Value |
|---|---|
| Orbit Life | Indefinite (solar sustained) |
| Return Accuracy | ±1.5 m (autonomous landing) |
| Energy Autonomy | 100% Solar (with battery buffer) |
| Cargo | 3–12 Tons |
Downloads & Files
Click to download the generated documents (white paper, business plan, and pitch deck).
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