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Demo & Free App Live Now · 2027 Full Launch

Chemistry for
the edge of
everything.

OrbitChem brings ChemeNova's AI formulation intelligence to space and aerospace applications — engineering materials for the most extreme environments on Earth and beyond. From thermal protection systems to radiation-stable lubricants, built to NASA MSFC and ESA ECSS standards.

OrbitChem™ · Research Targets
NASA MSFC
Material Standards
ESA ECSS
European Space Standard
LEO · GEO
Orbital Environments
Deep Space
Beyond GEO Applications
TPS
Thermal Protection Systems
Outgassing AI
ASTM E595 Compliance
2027
Target Platform Launch
IntelliForm Core
Intelligence Foundation
Thermal Protection Systems Outgassing Control · ASTM E595 Radiation-Stable Lubricants NASA MSFC Standards ESA ECSS Compliance Propellant-Compatible Adhesives Hypersonic Materials LEO · GEO · Deep Space Thermal Protection Systems Outgassing Control · ASTM E595 Radiation-Stable Lubricants
// Mission environment simulator

Where OrbitChem
operates.

Select a destination to read the material stressors OrbitChem formulates against — live telemetry drawn from real space-environment envelopes.

Low Earth Orbit
LEO · 200–2,000 KM · 51.6° INC
Nominal
Thermal Extreme
Radiation (TID)
Surface Chemistry
Pressure Regime
Mission Duration
Dominant failure mode
Critical standard
Recommended material classes
ENV-SIM · ChemeNova OrbitChem™ · REV 2.7
// Material categories

Four material domains.
One intelligence platform.

01 · Thermal

Thermal Protection Systems

AI-guided formulation of ablative heat shield materials, ceramic insulating tiles, and reusable TPS coatings. OrbitChem optimizes char formation rates, recession behavior, and structural integrity under hypersonic heat flux — all from composition alone.

  • Phenolic resin / silica ablator systems
  • PICA (Phenolic Impregnated Carbon Ablator) analogs
  • Low-density flexible ablators (LDEF-type)
  • Ceramic thermal barrier coatings (TBC)
  • Reusable surface insulation (RSI) tile materials
Peak heat flux1600°C
Char yieldHigh
ReusabilityRSI
02 · Adhesives

Structural & Outgassing-Controlled Adhesives

Precision formulation of epoxy, polyurethane, and silicone adhesive systems meeting ASTM E595 outgassing requirements. Every molecule evaluated for total mass loss (TML) and collected volatile condensable materials (CVCM) at 125°C/24h test conditions.

  • ASTM E595 TML < 1.0% / CVCM < 0.1% targeting
  • Cryogenic-service adhesives (-196°C to +150°C)
  • Propellant-compatible formulations (MON/UDMH/NTO)
  • Bondline adhesives for TPS tile-to-structure interfaces
  • Optical instrument bonding (vibration + thermal stable)
TML margin<1.0%
CVCM margin<0.1%
Cryo range−196°C
03 · Lubricants

Radiation-Stable Lubricants

Space-grade lubricant formulation for mechanisms operating in vacuum and high-radiation environments. Perfluoropolyether (PFPE) base fluid optimization, radiation dose tolerance modeling, and vapour pressure prediction at mission temperature extremes.

  • PFPE fluid and grease formulation optimization
  • Radiation dose tolerance (>1 MGy) prediction
  • Vapour pressure modeling at −200°C to +200°C
  • Anti-creep and migration control additive selection
  • MoS₂ and WS₂ dry-film lubricant binder systems
Dose tolerance>1MGy
Vapour press.Low
Temp range±200°C
04 · Functional Coatings

Spacecraft Coatings & Films

Specialized surface treatment formulations for thermal control, EMI shielding, and optical performance. Second-surface mirror coatings, black body paints, anti-static treatments, and atomic oxygen barriers — each formulated with full spectral and optical property prediction.

  • Thermal control coatings (α/ε ratio optimization)
  • Optical solar reflectors (OSR) backing coatings
  • Black body reference paints (Aeroglaze Z306-type)
  • Atomic oxygen barrier films (SiO₂/Al₂O₃ hybrid)
  • Anti-static and EMI shielding surface treatments
α/ε controlTuned
AO barrierSiO₂
Optical pred.Full
// Why this is hard

Space chemistry has no
room for trial and error.

01

No iterative debugging in orbit

Unlike terrestrial chemistry, space materials must perform flawlessly from the first deployment. There are no bench reformulations after launch. Every material decision is locked in at PDR/CDR — OrbitChem moves the screening loop to before the design review.

Target: Zero field reformulations
02

10–15 year mission lifetimes

Space materials must maintain performance for the duration of missions that span a decade or more. Long-term radiation dose accumulation, micrometeorite erosion, and thermal cycling fatigue are all design inputs — not failure modes to discover.

Mission duration: up to 15 years orbital
03

Outgassing contaminates optics

Even trace outgassing from polymers, adhesives, and coatings can deposit on optical lenses, solar cells, and thermal radiators — degrading performance by orders of magnitude. ASTM E595 compliance is mandatory, not optional.

ASTM E595: TML < 1.0%, CVCM < 0.1%
04

Radiation dose accumulation

Materials in LEO and beyond absorb ionizing radiation that degrades polymer chains, oxidizes lubricant base fluids, and shifts optical properties over time. Total ionizing dose (TID) prediction from molecular structure is a core OrbitChem capability.

LEO TID: 10–100 kRad/year (Al-shielded)
05

Propellant compatibility

Adhesives, seals, and coatings near propellant systems must be fully compatible with hydrazine, NTO, MON, and UDMH — highly corrosive and toxic propellants that attack standard polymers. Every material in the propellant pathway requires individual qualification.

Propellants: MMH / N₂H₄ / NTO / MON-3
06

Cryogenic property retention

Cryogenic propellant tanks, deep space probe components, and cryo-cooled detector systems require materials that remain flexible, adhesive, and dimensionally stable at liquid nitrogen and helium temperatures — without becoming brittle or delaminating.

Operating range: −270°C to +1,600°C
// Live outgassing qualification

No room for trial and error?
Screen a material right here.

A working ASTM E595 outgassing check — the same screening every space-bound material must pass. Pick a material or move the sliders; the flight verdict updates live.

Total Mass Loss · TML 0.78%
Scale 0–3.0% · NASA limit ≤ 1.00%
Collected Volatile Condensable Materials · CVCM 0.040%
Scale 0–0.5% · NASA limit ≤ 0.10%
TML vs limitPass
CVCM vs limitPass
Qualified for flight
Both metrics within ASTM E595 screening limits.
ASTM E595 · 125 °C / 24 h / 10⁻⁶ torr · TML ≤ 1.00% · CVCM ≤ 0.10%
// Available now — free

Try OrbitChem
today.

No account required. No install. Two ways to access the platform while the full 2027 launch is in development.

01 · Static Demo

Interactive
Calculator Suite

chemenova.com/orbitchem/demo

Three fully client-side calculators running live in your browser. No server, no account, no install. ASTM E595 outgassing estimator, TID radiation modeler, and Coffin-Manson thermal cycling predictor — all physics-based.

  • ASTM E595 outgassing calculator (TML / CVCM)
  • Total ionising dose (TID) radiation modeler
  • Coffin-Manson thermal cycling fatigue predictor
  • AI material intelligence brief (mission-specific)
  • 38 space-grade materials database
02 · Full Platform

9-Module
Streamlit App

orbitchem.chemenova.com

The complete OrbitChem platform running on Hugging Face Spaces. All 9 modules including the Full Qualification Suite, SpaceChem-AI molecular screening for Type II Civilization candidacy, and the Autonomous Molecular Digital Twin (AMDT).

  • Full Qualification Suite (outgassing + radiation + thermal)
  • SpaceChem-AI — Type II Civilization molecular screening
  • ⚡ Type II Integrated Qualification (SMILES → full report)
  • AMDT — Autonomous Molecular Digital Twin
  • PDF proposal export — ChemeNova branded

Built to the
most demanding
standards on Earth.

OrbitChem is architected against the space and aerospace material standards enforced by NASA, ESA, and the defense industry. No other formulation platform addresses this regulatory landscape.

NASA MSFC-SPEC-250

Protective Finishes for Space Vehicles

Primer and topcoat systems for structural and thermal protection in space environments

ESA ECSS-Q-ST-70

Space Product Assurance — Materials

Outgassing, flammability, and compatibility requirements for all materials in ESA missions

ASTM E595

Total Mass Loss & CVCM

Screening test for material outgassing in space environments — TML and CVCM limits enforced

MIL-L-27694

Lubricating Oil, Aircraft Turbine Engine

High-performance aerospace lubricant qualification standards

ASTM E1559

Contamination Outgassing Characteristics

Rates and activation energies of outgassing species from spacecraft materials

ECSS-E-HB-32-22A

Insert Design Handbook

Adhesive systems for metallic inserts in composite space structures

// Research waitlist

Shape OrbitChem
from the ground up.

OrbitChem is in active research. Join our waitlist and we'll involve you in the technical development — your requirements become our roadmap. Space materials engineers, aerospace primes, and research institutions welcome.

Or email directly: [email protected]

The universe is
waiting for better chemistry.

OrbitChem is available now as a free demo and full Streamlit app. The demo runs entirely in your browser — no account needed.

Try OrbitChem Demo → Free App → Research Partnership