VYORDEEP SPACE SYSTEMS
VYOR / RESEARCH STAGE / GERMANY / 2026

Find it.Reach it.Know it.

VYOR is developing the low-cost autonomous prospecting and material-acquisition stack required to characterize and exploit small Solar System bodies.

WORKING THESISCharacterize → rendezvous → interact → acquire → process.
01
AUTONOMOUS OPTICAL NAVIGATIONSPECTRAL PROSPECTINGDEEP-SPACE AVIONICSLOW-GRAVITY MATERIAL ACQUISITIONREPEATABLE MISSIONSAUTONOMOUS OPTICAL NAVIGATIONSPECTRAL PROSPECTINGDEEP-SPACE AVIONICSLOW-GRAVITY MATERIAL ACQUISITIONREPEATABLE MISSIONS
01 Mission thesis

Before you mine it,you have to understand it.

Mining is not the first mission. Reliable characterization is.

Our roadmap begins with the capabilities that survive every later phase: autonomous target acquisition, optical navigation, spectral sensing, onboard decision-making, deep-space communications, proximity operations and controlled interaction with low-gravity surfaces.

The company is built around turning one-off exploration capabilities into a compact, repeatable commercial stack for small-body missions.

01 / AUTONOMY

Autonomy first

As latency increases, spacecraft must make more navigation and safety decisions without continuous ground intervention.

02 / PROSPECTING

Prospect before extracting

Remote sensing reduces uncertainty before expensive contact, excavation and processing hardware is committed.

03 / HERITAGE

Flight heritage compounds

Every early mission should retire a failure mode that appears again on the eventual resource mission.

04 / FOCUS

Own the differentiator

Buy commodity spacecraft hardware early. Own the autonomy, sensing, mission software and acquisition architecture.

02 Technology stack

Four systems.One mission stack.

The early company is not a refinery in space. It is the enabling layer that makes characterization and controlled interaction inexpensive enough to repeat.

A / 01NAVIGATION

Autonomous navigation

Optical target acquisition, relative navigation, autonomous approach, safe-mode logic and fault-aware planning.

Long-range detectionFeature navigationOnboard guidance
B / 02SPECTROSCOPY
BAND

Spectral prospecting

Compact visible and near-infrared sensing designed to classify candidate materials and map compositional variation before contact.

VNIR / SWIRCalibrationComposition inference
C / 03SPACECRAFT

Deep-space platform

High-reliability avionics, power, propulsion, communications and operations built around small-body missions rather than generic LEO duty cycles.

FDIRLong-range commsMobility
D / 04ACQUISITION

Material acquisition

Low-reaction-force contact, capture and excavation concepts designed for environments where the tool can push the spacecraft away from the surface.

Contact dynamicsContainmentRegolith capture
03 Mission roadmap

Earn the next mission.

A staged program from bench testing to asteroid interaction. Dates are planning targets, not claims. Each phase is designed to retire a specific class of risk.

Asteroid Bennu — NASA Scientific Visualization Studio
PHASE 00 / NOW2026–27

Foundation

Target-selection database, autonomous tracking, spectral breadboard, systems engineering, regulatory strategy and first low-gravity acquisition tests.

PHASE 012027–28

Prospector-0

Hosted orbital payload proving sensing, calibration, autonomous target acquisition, onboard processing and reliable space-to-ground operations.

ESA Hera concept near Didymos
PHASE 03–042029–34

Deep-space prospector

Flyby first, then rendezvous: deep-space communications, long-duration reliability, optical navigation, close characterization, resource mapping and proximity operations.

00
2026–27

Laboratory stack + mission architecture

Mission design, target database, sensing breadboards, autonomy software, systems engineering and funding/regulatory groundwork.

ConOpsTarget DBBench stack
01
2027–28

Hosted payload — Prospector-0

Prove the differentiated payload and autonomy stack in orbit before taking responsibility for the entire spacecraft bus.

Flight payloadCalibrationTracking
02
2028–29

Dedicated 6U / 12U — Prospector-1

Integrate propulsion, precision ADCS, safe modes and more autonomous operations into a spacecraft controlled end to end.

Own busGNCFDIR
03
2029–32

Near-Earth asteroid flyby

Demonstrate deep-space communications, optical navigation, long-duration operations and remote spectral characterization.

Deep spaceFlybySpectra
04
2031–34

Asteroid rendezvous

Match velocity, map shape and spin, characterize surface properties and identify candidate interaction sites.

RendezvousProximity opsMap
05
2033–36

Miner-0 — controlled contact + acquisition

Demonstrate surface interaction and kg-scale capture while measuring reaction forces, dust behavior and material properties.

TouchAcquireContain
06
2035+

Processing demonstration + scaling

Select the extraction chain after ground truth exists. Prove processing at kilograms before committing to industrial-scale transport or refining.

ProcessYieldRepeat
04 Mission heritage

The physics is proven. The economics are not.

NASA, JAXA and ESA missions demonstrate the sequence: find, approach, map, touch, sample and operate around small bodies. The commercial problem is to compress mission cost, time and operational complexity.

Asteroid Bennu
NASA Scientific Visualization Studio / OSIRIS-REx
NASA / OSIRIS-REx

Characterize → touch → return.

A reference architecture for turning remote observations into site selection, physical contact and sample return.

Asteroid Ryugu imaged by Hayabusa2
ISAS/JAXA — CC BY 4.0-compatible source
JAXA / HAYABUSA2

Low-gravity surface interaction.

Multiple surface interactions and returned samples provide ground truth for what remote sensing can and cannot tell us.

ESA Hera concept at Didymos
ESA – Science Office, CC BY-SA 3.0 IGO — display crop
ESA / HERA

European small-body operations.

Autonomy, close characterization and CubeSat-enabled investigation around a binary asteroid system.

Mission imagery is presented as technical heritage and context. VYOR is independent and is not affiliated with or endorsed by NASA, ESA, JAXA, DLR or their mission partners. Before commercial publication, re-check each source licence and retain the detailed attribution file.

05 Operating thesis

Every mission must retire real risk.

01
Unknown objectTarget priors + remote observations
02
Characterized targetShape, spin, spectrum, surface state
03
Controlled interactionRendezvous, proximity operations, contact dynamics
04
Acquired materialCapture yield + physical ground truth
05
Resource productProcessing, transport and customer economics
06 Building from Europe

The first mission starts before launch.

We are at the research and architecture stage. We are interested in conversations with spacecraft engineers, GNC researchers, planetary scientists, spectroscopy teams, low-gravity robotics groups and early deep-tech partners.

Start a conversation Configure the final VYOR email address after securing the company domain.