Prototype Development

ResiliRad-Bio AI

Physics-Informed Radiation Exposure and Biological-Response Intelligence for Human Spaceflight

ResiliRad-Bio AI connects solar and space-weather observations, radiation-monitor measurements, mission trajectory and shielding conditions, radiation dose, and biological-response evidence to support human spaceflight research, mission planning, and radiation-risk assessment.

Explore Radiation Data View Biological Evidence

Prototype notice:All displayed measurements, mission states, event records, biological matches, and AI assessments are simulated or demonstration data unless a verified source is explicitly identified. They are not astronaut medical records or clinical predictions.

1. Mission Environment Overview

Mission and radiation environment status

Mission Region

LEO

Demonstration selection

Mission Phase

Orbital Operations

Simulated context

Radiation Environment

Elevated

Prototype classification

Solar Activity

Moderate

Demonstration data

Radiation Event

No active alert

Not operational

Data Availability

Prototype feeds

APIs not yet connected

2. Radiation Exposure Summary

Exposure metrics

Demonstration-only metrics showing the planned structure for verified dosimetry, particle flux, cumulative exposure, and uncertainty products.

Absorbed Dose

0.42mGy

Simulated demonstration value

Dose Rate

18.6µGy/hour

Simulated demonstration value

Dose Equivalent

0.74mSv

Simulated demonstration value

Cumulative Mission Dose

12.8mSv

Simulated demonstration value

Particle Flux

2.4 × 10³particles/cm²/s

Simulated demonstration value

Exposure Uncertainty

±18%

Simulated demonstration value

3–4. Time History and Space-Weather Drivers

Radiation timeline and upstream context

Radiation Timeline

Interactive chart placeholder
Planned series: dose rate, proton flux, electron flux, SEP activity, and detected events.

Space-Weather Drivers

Solar flare activityModerate — demonstration status

CME statusNo verified event connected

Solar energetic particlesPrototype elevated classification

Solar-wind speedDemonstration: 485 km/s

IMF conditionsDemonstration southward interval

Geomagnetic activityDemonstration: active

5. Mission and Trajectory Context

Exposure in mission context

Spacecraft Position

LEO demo orbit

Mission Phase

Orbital operations

Shielding

Reference config.

Crew Status

IVA demo

Instrument Location

Cabin reference

6. Radiation Instrument Data

Instrument and platform measurements

Instrument	Platform	Measurement	Time Range	Dose Rate	Particle Flux	Quality	Source
Demo Dosimeter A	LEO research platform	Dose rate	Last 24 hours	18.6 µGy/h	2.4 × 10³ cm⁻²s⁻¹	Prototype	Simulated
Particle Telescope B	Reference instrument	Proton/electron flux	Last 24 hours	—	1.8 × 10³ cm⁻²s⁻¹	Demonstration	Placeholder
NASA RadLab	Planned integration	Radiation measurements	Future connection	Not connected	Not connected	Planned	NASA RadLab

7. Biological-Response Evidence

Mission-exposure evidence matching

Planned integration of GeneLab and OSDR studies with exposure characteristics, biological models, tissues, molecular responses, and similarity metrics.

Study	Radiation Type	Dose	Dose Rate	Model	Tissue/Cells	DE Genes	Pathways	Evidence	Mission Similarity
OSDR demonstration study	Mixed ionizing radiation	0.5 Gy	Acute	Cell culture	Epithelial cells	Prototype set	DNA damage; oxidative stress	Moderate	Partial
GeneLab demonstration study	Protons	0.3 Gy	Low dose rate	Rodent	Liver tissue	Prototype set	Immune regulation; repair	Exploratory	Low–moderate

Research-use notice: Biological-response results are research evidence and are not individual astronaut diagnoses or clinical predictions.

8. AI-Generated Exposure Assessment

Explainable analyst summary

“The detected radiation environment shows an elevated proton contribution relative to the quiet-time baseline. Available biological studies with comparable exposure characteristics indicate potential relevance to DNA-damage response, oxidative stress, immune regulation, and cellular-repair pathways. Additional validation is required because of differences in dose rate, radiation quality, shielding, biological model, and sampling time.”

ConfidenceModerate / Demo

Major AssumptionsReference shielding

Model VersionPrototype 0.1

ProvenanceSimulated + literature schema

Limitations: No verified live astronaut, dosimetry, RadLab, trajectory, or molecular dataset is connected in this demonstration.

9. Event Analysis

Detected radiation events

Event ID	Start	End	Type	Peak Dose Rate	Cumulative Dose	Solar Association	Confidence	Status	Actions
RB-DEM-001	2026-07-12 03:20 UTC	2026-07-12 05:05 UTC	Proton enhancement	31.2 µGy/h	0.054 mGy	Demonstration SEP context	0.72	Prototype review
RB-DEM-002	2026-07-10 19:40 UTC	2026-07-10 20:25 UTC	Electron enhancement	24.1 µGy/h	0.018 mGy	Geomagnetic activity	0.64	Unvalidated

10. Data Integration Architecture

From space-weather drivers to mission decisions

Solar and Space-Weather Data

↓

Particle Environment

↓

Mission Trajectory and Shielding

↓

Radiation Instrument Measurements

↓

Dose and Exposure Reconstruction

↓

GeneLab and OSDR Evidence Matching

↓

Mission and Research Decision Support

11. Development Status

Prototype roadmap

RadLab data integration

Space-weather data harmonization

Radiation-event detection

Dose and uncertainty analytics

GeneLab/OSDR evidence integration

SDSI mission-data integration

Physics-informed AI models

Mission-specific decision-support tools

Current Stage: Prototype / Research and Development