🗺 Surface Map
🚶 Marswalk Plan
📡 NASA Data Layers
🌪 Mars Weather
⛰ Terrain Profile
🔬 Science Targets
⚠ Hazard Map
📅 EVA Timeline
📋 Mission Brief
💬 AI Chat
Mars Surface Map — Jezero Crater
18.4°N
Latitude
77.7°E
Longitude
−2,900m
MOLA Elevation
−63°C
Surface Temp
Tau 0.5
Dust Opacity
MOLA Topo
Minerals (CRISM)
Thermal (THEMIS)
Route
Hazards
Science Targets
HiRISE Coverage
🔴 MARSWALKAI SITE OVERVIEW WATSONX
Select a landing site and click "Plan Marswalk" to generate an AI-powered surface route optimised for science, safety, and EVA duration. Powered by IBM watsonx Granite with NASA mission data integration.
Planned Marswalk Route
Generate a marswalk plan to see the AI-optimised route with waypoints, science stops, and hazard avoidance.
🚶 MARSWALK ROUTE PLAN WATSONX AI
Click "Plan Marswalk" in the sidebar to generate a detailed, AI-optimised route plan for your EVA.
Integrated NASA Science Data
MOLA Topography
Mars Orbiter Laser Altimeter · MGS
−2,900 m
Mars Global Surveyor MOLA provides 1/128° resolution elevation data. Jezero Crater floor shows a ~50m deep lacustrine basin ideal for ancient sediment sampling.
CRISM Mineralogy
Compact Reconnaissance Imaging Spectrometer · MRO
Mg-carbonate detected
CRISM spectral data reveals magnesium carbonates and olivine-bearing units in the Jezero delta — prime biosignature preservation targets. Hydrated silica also detected.
THEMIS Thermal Inertia
Thermal Emission Imaging System · Mars Odyssey
420 TIU
Thermal inertia 420 J m⁻² K⁻¹ s⁻⁰·⁵ indicates compact, possibly cemented regolith. EVA traversability is GOOD. Avoid low-TI zones (dusty regolith, potential trafficability hazard).
MCS Atmospheric Profile
Mars Climate Sounder · MRO
700 Pa surface pressure
Current atmospheric pressure 700 Pa (0.7% Earth sea level). Dust optical depth τ = 0.5 (clear). Temperature inversion detected 20 km altitude. EVA weather: GO.
HiRISE High-Res Imagery
HiRISE Camera · MRO (25 cm/px)
25 cm/px resolved
HiRISE 25 cm/pixel resolution reveals boulders >0.5m diameter along proposed route. Two boulder fields flagged as route diversions. Delta front scarp visible at WP-4.
Perseverance Ground Truth
Mars 2020 Rover · Sol 1200 Data
1,200+ sol traverse
Perseverance rover Sol 1200 traverse data validates route terrain models. Regolith shear strength ~7 kPa. No significant sand traps detected in primary EVA zone. 24 sample tubes cached.
📡 DATA INTEGRATION ANALYSIS WATSONX AI
NASA multi-mission data displayed above. Click "Plan Marswalk" to generate an AI analysis integrating all layers for your specific EVA objectives.
Mars Weather — Jezero Crater
−63°C
Surface Temperature
Range: −80°C night / −20°C midday peak. EVA window: 09:00–15:00 LMST
12 m/s
Wind Speed (surface)
Prevailing NW direction. Gusty in afternoon. EVA limit: 25 m/s. Current: SAFE
Tau 0.5
Dust Optical Depth
Clear conditions (τ < 1.0). Seasonal dust storm probability 18%. Solar power: 92% nominal
700 Pa
Atmospheric Pressure
0.7% Earth sea level. Suit design minimum 41 kPa internal. All EVA systems: NOMINAL
590 W/m²
Solar Irradiance
43% of Earth equivalent at 1.52 AU. UV Index: EXTREME — suit UV protection required
3 detected
Dust Devils (today)
3 dust devils detected in 20 km radius. Diameter est. 50–120 m. Avoid dust devil tracks
10-Sol Forecast
🌪 WEATHER ANALYSIS MCS + WATSONX AI
Click "Weather Report" to generate an AI-powered EVA weather assessment based on Mars Climate Sounder data and seasonal dust storm models.
Terrain Elevation Profile (MOLA)
Route Max Slope
MOLA + HiRISE derived
11.3°
Maximum slope along planned route. EVA suit mobility limit: 20°. Recommended limit for safety: 15°. Current route: WITHIN LIMITS.
Elevation Change
HiRISE DTM · 1m resolution
+42m / −18m
Total ascent 42m, descent 18m along 3.2 km route. Energy expenditure estimate: 420 kCal additional above baseline for suited astronaut.
Surface Trafficability
Perseverance RIMFAX + terrain data
GOOD
RIMFAX ground-penetrating radar shows competent bedrock within 50 cm along primary route. No subsurface voids detected. Regolith: compact.
Regolith Composition
CRISM + APXS Heritage Data
Basaltic + Mg-Carb
Primary basaltic regolith with Mg-carbonate patches at delta margin. Olivine-rich units near WP-4. Perchlorate concentration: 0.5% (standard Mars surface — suit contamination protocol required).
Science Targets Along Route
P1
Jezero Delta Front Scarp
18.4847°N, 77.5840°E · WP-4 · Distance: 2.1 km
The most compelling biosignature preservation target on Mars. CRISM detects Mg-carbonates and hydrated silica — identical to environments where early Earth life was preserved. Priority 1 sample collection.
Instruments: SHERLOC (Raman), PIXL (XRF), drill sampling, hand lens imaging
P1
Olivine-bearing Bedrock Outcrop
18.4720°N, 77.5910°E · WP-6 · Distance: 2.8 km
Olivine-bearing units detected by CRISM. Unweathered olivine indicates rapid burial, preserving potential organic compounds. Key sample for establishing timeline of Mars water activity.
Instruments: SHERLOC, hand sample, field notebook, context imaging
P2
Perseverance Sample Cache Site
18.4651°N, 77.6103°E · WP-8 · Distance: 3.2 km
Location of 10 sample tube depot cached by Perseverance rover. Tube retrieval enables Earth return of carefully curated samples. High mission return value — extends Perseverance science program.
Instruments: Sample tube retrieval, visual documentation, GPS survey
P2
Lacustrine Sedimentary Unit
18.4590°N, 77.5760°E · WP-3 · Distance: 1.5 km
Fine-grained lacustrine sediments mapped by CRISM. These represent the deepest water-deposited layers — highest potential for preserved organics. Stratigraphic section measurement needed.
Instruments: Drill, PIXL, sediment texture analysis, stratigraphy logging
P3
Dust Devil Track Survey
18.4800°N, 77.6400°E · WP-10 · Distance: 4.0 km
Active dust devil tracks expose fresh subsurface material. Opportunity to characterise unweathered regolith at depth. Also collects MEDA wind/dust data for future EVA planning models.
Instruments: Scoop sampling, MEDA calibration, soil mechanics test
🔬 SCIENCE BRIEF WATSONX AI
Click "Science Brief" in the sidebar to generate an AI-powered science prioritisation and instrument recommendation for your EVA objectives.
Hazard Assessment
Solar Radiation — SPE Alert
Space weather forecast shows elevated solar energetic particle flux. During EVA, crew will receive ~0.8 mSv/hour surface dose (GCR + scattered radiation). Limit EVA duration if SPE event triggers (>10 mSv threshold). Storm shelter location: Base Camp (200m SW, 3 min return).
Source: NASA Space Weather · NOAA SWPC real-time data
Dust Devil Field — SE Quadrant
HiRISE detects active dust devil tracks in SE portion of EVA zone. Dust devils at Jezero average 50–200m diameter, wind speeds 25–35 m/s. Route WP-9 → WP-10 passes through high-frequency zone. Recommend morning EVA scheduling (before 11:00 LMST) when convective activity is minimal.
Source: HiRISE seasonal monitoring · MEDA dust devil sensor data
Boulder Field — WP-3 to WP-4
HiRISE 25 cm imagery reveals dense boulder field (>50 boulders/100m²) between WP-3 and WP-4. Boulders 0.5–2.0m diameter. Route detours 180m west to avoid. Original straight-line path slope of 14° also exceeds recommended limit. Alternate route adds 12 minutes to EVA schedule.
Source: HiRISE ESP_058795_1985 · Perseverance AutoNav terrain data
Soft Regolith Zone — WP-7
THEMIS low thermal inertia anomaly at WP-7 coordinates indicates unconsolidated dust deposit estimated 30–60 cm depth. Risk of astronaut sinking / reduced mobility. RIMFAX data shows fine-grained particle accumulation in topographic low. Mark as AVOID and route around perimeter (+45m route addition).
Source: THEMIS TI anomaly map · RIMFAX subsurface radar (Sol 850–900)
Perchlorate Contamination Risk
Mars surface perchlorates (average 0.5 wt%) detected across EVA zone by Phoenix lander heritage data. All sample handling requires contamination protocol. Do not allow regolith contact with bare skin or suit life-support inlet. Decontamination station required at airlock re-entry. Perchlorate is a health hazard at >0.1 mg/kg body weight.
Source: Phoenix WCL instrument data · MECA chemistry analysis
Thermal Stress — Suit Management
Rapid temperature cycling: surface warms from −80°C dawn to −20°C midday peak, then rapid cooling. EVA suit thermal regulation load increases dramatically in afternoon. Schedule primary EVA 08:00–14:00 LMST. Avoid EVA at night (radiative cooling 100 W/m² from suit). Battery drain rate increases 23% below −50°C.
Source: REMS temperature data (Curiosity) · InSight HP3 thermal measurements
⚠ HAZARD INTELLIGENCE WATSONX AI
Click "Assess Hazards" to generate a comprehensive AI hazard assessment integrating NASA surface and orbital data for your specific EVA route and conditions.
EVA Timeline — Gantt Schedule
LMST LOCAL MARS TIME — EVA START 09:00
EVA Resource Budget
Real-time consumption model
O₂: 0.84 kg used
Per astronaut: 0.14 kg/hr × 6 hr = 0.84 kg. Carried: 1.26 kg (33% reserve). Emergency reserve: 0.42 kg. Battery: 86% consumed. All nominal for planned EVA.
EVA Window Analysis
MCS + MEDA thermal data
09:00–15:00 LMST
Optimal window: temperature above −70°C, wind below 18 m/s, solar power above 85% nominal. Dust devil activity low before 11:00 LMST. Schedule high-priority stops in first 3 hours.
Science Time Allocation
Instrument time budget
156 min science
SHERLOC Raman: 48 min · PIXL XRF: 60 min · Drill sampling: 48 min · Total planned science: 156 min out of 360 min EVA. Traverse/logistics: 204 min.
Route Distance Summary
HiRISE + MOLA derived
4.5 km total
Outbound 2.8 km to deepest science target. Return 1.7 km (modified route avoids soft regolith). Average walking speed: 0.8 km/hr in EVA suit on Martian terrain.
📅 EVA TIMELINE ANALYSIS WATSONX AI
Click "Plan Marswalk" to generate an AI-optimised EVA timeline with phase scheduling, go/no-go windows, and resource consumption projections.
Formal EVA Mission Brief
EVA OPERATIONS ORDER
JEZERO CRATER · MARS SURFACE OPERATIONS
NASA APPROVED FORMAT
AI GENERATED
Mission Sol
—
EVA Duration
6 hours
Status
DRAFT
1. MISSION OVERVIEW
Generate a Marswalk plan to populate this section with AI-authored mission overview, objectives, and success criteria.
2. SCIENCE OBJECTIVES
Integrated NASA multi-mission data (CRISM, MOLA, HiRISE, Perseverance) will populate priority science targets, instrument plan, and sample strategy.
3. HAZARD SUMMARY
Click "Assess Hazards" to populate with radiation, terrain, atmospheric, and chemical hazard assessments from NASA data.
4. WEATHER & GO/NO-GO
MCS atmospheric data, dust storm forecast, and EVA weather window will populate here after generating weather report.
5. NASA DATA SOURCES
MOLA v5 · CRISM TRDR · THEMIS TES · HiRISE ESP · MCS v5.3 · Perseverance MEDA/RIMFAX · Curiosity REMS · InSight HP³ · Phoenix MECA · NOAA SWPC space weather
6. EMERGENCY PROCEDURES
SPE alert → abort immediately, shelter in habitat (3 min). Suit failure → EVA partner assist, immediate return. Visibility < 50m → halt, shelter in place, await Mission Control go-ahead. Comms loss → return to base camp per pre-planned abort route.
📋 MISSION BRIEF WATSONX AI
Click "Generate Full Mission Brief" to produce a formal, submission-ready EVA operations order integrating all NASA data layers — suitable for mission planning review boards.