The European orbital compute thesis
12 slides. Cold-outreach pitch. Press P or use the button below to save as PDF. Canonical pitch lives at /investors.
high machines · investor deck
The European orbital compute thesis
Architecture lock by mid-2027 · €2–5M seed · 18-month window
Jan-Peter · PhD, AI4CE concurrent engineering · high machines · 2026-06-30
01 · Problem
Earth-bound compute can't scale
- Global data centre market ~$1.1T by 2035 — power, cooling, and density are the binding constraints on the ground.
- AI demand doubles every ~9 months; latency to LEO is ~150× faster than GEO; energy in space is ~8× more productive.
- The regulatory window is being written right now — ITU 2027, EU Space Law — and the architectures are being designed right now.
02 · Solution
Hub-and-spoke orbital compute for European sovereign AI
- Target architecture: 120 satellites @ 600 km @ 100 TFLOPS each, anchored on a European sovereign-AI workload.
- Mission-architecture design via deep reinforcement learning — the AI4CE PhD applies deep RL to constellation design, a capability 30-year engineering cultures cannot replicate.
- The seed funds the architecture lock + regulatory lane; the architecture lock justifies the Series A.
03 · Why this
The physics, the latency, the energy, the regulatory window
- Above the atmosphere, solar is roughly 8× more productive, heat sheds by radiation, vacuum is free insulation.
- LEO is ~150× faster than GEO for space-data round-trips — and that's the better problem.
- The regulatory window (ITU 2027, EU Space Law) is being written right now — whoever locks the architecture by mid-2027 sets the standard.
04 · Why now
The 2025–2027 phase shift · the 18-month window
- Between late 2025 and early 2026, orbital compute went from a slide in an ESA briefing to a product with customers and a launch manifest.
- Starcloud trained an LLM in space (Dec 2025); Axiom launched the first two ODC nodes to the ISS (Jan 2026); Google "Project Suncatcher" announced an 81-satellite TPUs-in-LEO constellation (early 2027).
- Europe has ~18 months to pick a lane.
05 · Why us
Why a young solo founder can win the lane that the primes don't want
- OHB has a 40-year track record. Airbus Defence and Space launches sovereign constellations. EnduroSat has the smallsat supply chain locked. They could do orbital compute. They won't.
- Orbital compute is 100% of our mission and ~1% of theirs; they run 5–10 year cycles; the opportunity is an 18-month window.
- The actual unfair advantage is the AI-native methodology — the AI4CE PhD applies deep RL to mission-architecture design.
- We get the market because the primes wait for proven demand. The 18-month window is for venture-funded startups to define the architecture.
06 · The market
TAM / SAM / SOM — sized today, sized defensibly
TAM
~$1.1T by 2035
Global data centre market (Precedence Research, 2026). Orbital-DC addressable slice is a fraction — but meaningful.
SAM
~$35B by 2030
Orbital data centre market (Markets-and-Markets + Yahoo Finance analyst consensus, 2026). AI data-centre slice ~$200–500B by 2032 (Grand View Research, 2026).
SOM
~$2–5B by 2032
European sovereign-AI in our orbit + SLA profile.
07 · Traction
What we've shipped
User stories shipped
55 of 62
All 4 Sprints closed (foundation + story + explore + polish); 55 US shipped incl. US30 hub-and-spoke (4 audience pages live).
Test coverage
550 unit + 6 e2e
100% green on every ship; the 6 e2e tests regression-gate the original orbit-visualization bug.
Published research
6 AI4CE papers
Deep RL for concurrent engineering — the methodological foundation of the company.
Competitive landscape
11 profiles mapped
Verified competitor profiles, single source of truth (markdown bind-mount; updates show up on next reload, no rebuild).
08 · Team
Solo founder + AI agent fleet
- Jan-Peter — founder. PhD in AI4CE concurrent engineering; deep RL for mission-architecture design. 6 published papers, 1 ESA CDF collaboration.
- OpenClaw agent fleet. In-house AI engineering agent (the same one writing this deck) — handles the engineering surface area a 4-person team would otherwise own. Self-improving; tracked via the BACKLOG/CHANGELOG discipline.
- EU regulatory network. Bundesnetzagentur authorisation pathway + ESA partnership status + 4 framework buckets per the US22 design review.
- Advisors TBD. The seed funds the first two senior hires (mission lead + regulatory lead).
09 · The ask
€2–5M seed to lock the architecture and the lane
We are at the post-research, pre-architecture stage. The deep-dive is done. The competitive landscape is mapped. The regulatory path is sketched. The engineering trade-offs are understood.
What €2–5M buys (€3M mid-point, illustrative):
- €1.2M FTE — 4 engineers × 2 years (mission design + RL ops + regulatory + EU partnerships).
- €0.6M spectrum + regulatory — ITU filings, EU Space Law readiness, BNetzA authorisation.
- €0.4M simulation stack — the "digital twin" of the 4-tier orbit constellation.
- €0.2M legal + corporate — entity setup, IP assignment, contract templates.
- €0.6M reserve — 24+ months of pure-software runway. Hardware spend is the Series A.
10 · Comparable rounds
Stage-fit, not headline-grab
- Starcloud: $170M Series A (March 2026) at a $1.1B valuation. The headline US orbital-AI Series A.
- US orbital-AI competitors (Axiom Space, Kepler Communications, Project Suncatcher, Sophia Space) have raised $100M+ each.
- We are raising €2–5M seed — an order of magnitude below the Series A's we've seen in this space. The seed funds the architecture lock that justifies the Series A math.
11 · Honest unknowns
What the seed funds the resolution of
- The anchor customer. Exploratory conversations with European hyperscalers and sovereign-AI programmes; SLA-defining conversation post-funding.
- The launch provider. Trade study pending architecture lock: SpaceX Falcon 9, Rocket Lab Neutron, Arianespace Vega-C.
- The radiation-hardening cost curve. 12-month vendor conversation; rad-hard vs COTS-with-shielding trade-off.
- The first-flight milestone. Hardware spend is post-architecture-lock, post-funding; the seed funds the design loop, not the flight.
30-min call → jan-peter@highmachines.space