Atlas Space University

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The Atlas Space Ecosystem

It takes an entire ecosystem to support two astronauts. Which role will you play?

Satellite Engineer Space Medicine Specialist Rocket Propulsion Scientist Space Lawyer Astrobiologist Space Architect Space AI Developer GIS Analyst Space Business Consultant Astronaut Candidate

Master of Science in Space Science

A 12-month intensive interdisciplinary graduate program accredited under ECTS rules.

M101: Space Systems

Satellite sub-systems, cleanroom FlatSat integrations, and launch load dynamics.

M102: Space Law & Policy

Outer Space Treaty, national regulations, ITAR audits, and frequency allocations.

M103: Space Informatics

Remote sensing, SAR imagery, crop ML classifications, and GEE architectures.

M104: Space Life Sciences

Space medicine, radiation mitigation, closed-loop ECLSS, and space agriculture.

Operational Milestones

Roadmap to launching Atlas Space University and sending the first Moroccans to space.

Q1 2027

Foundations & Selection

Execution of contracts with Axiom Space, starting national selection campaign for astronaut candidates.

Q2 2027

Accreditation & Staffing

Filing academic accrediting requests with ANEAQ and recruiting permanent academic Chairs.

Q3 2027

Dorms & Labs Setup

Groundbreaking at Marrakech campus, building rammed-earth structures, and installing cleanroom HEPA filters.

Q4 2027

First Class Launch

Inaugural cohort of 100 students arrives on campus. Ground station satellite telemetry links active.

Strategic Funding Projections

Phased CapEx and OpEx investments over the first 5 years ($150 Million Total).

YEAR 1 BUDGET

35,000,000 USD

Admissions & Eligibility Tool

Check your ECTS credit alignment and scholarship category eligibility instantly.

Academic Background

Nationality / Residency

ISO 7 Cleanroom Monitoring

Interactive simulation of real-time HEPA filtration and particulate control in our satellite assembly lab.

HEPA STATUS

ACTIVE

Satellite Orbit Simulator

Visualize satellite orbits and telemetry ground cover paths calculated in our Informatics Lab.

Target Orbit

Velocity 7.6 km/s

Period 95 mins

Orbital Trajectory Planner

Plan Hohmann transfers and evaluate delta-V budgets for CubeSats in our Propulsion Lab.

Target Altitude (km) 500 km

Velocity 7.61 km/s

Delta-V Required 82 m/s

Payload Mass Budget Planner

Configure satellite component mass allocations and track launch margins in our Space Systems Lab.

Avionics & Bus (kg) 15 kg

Science Payload (kg) 10 kg

Total Mass 25 / 50 kg

Margin Status NOMINAL

Solar Array Efficiency Simulator

Optimize solar array incident angles and evaluate cell technology performance in our Space Systems Lab.

Tilt Angle (deg) 0 deg

Cell Material

Power Output 245 W

Array Efficiency 18%

Spacecraft Power Budget

Configure instrument draws and verify battery depth-of-discharge parameters in our Space Systems Lab.

Avionics Load (W) 40 W

Payload Load (W) 80 W

Net Margin +125 W

Battery State CHARGING

Battery State-of-Charge

Analyze depth-of-discharge parameters and battery cell health profiles over simulated eclipse periods.

Battery Chemistry

Eclipse Duration (mins) 15 mins

State-of-Charge (SoC) 87.5%

Safety Status NOMINAL

Thermal Radiator Equilibrium

Simulate thermal balance loops and radiator equilibrium temperatures in our Space Systems Lab.

Orbit Phase

Radiator Coating

Equilibrium Temp 298 K

Thermal Margin SAFE

Propellant Combustion Simulator

Simulate chemical combustion nozzle exhaust and evaluate specific impulse parameters in our Propulsion Lab.

Propellant Mix

Specific Impulse (Isp) 311 s

Combustion Temp 3,570 K

Radiation Shielding Simulator

Analyze micro-sievert exposure rates and evaluate multi-material barriers in our Space Life Sciences Lab.

Shielding Material

Absorbed Dose 100%

Safety Status CRITICAL

Closed-Loop Life Support (ECLSS)

Analyze recycling loops and biomass systems in our Space Life Sciences Lab.

Greywater Processor

Sabatier Reactor

Algae Photobioreactor

Water Recovery 93%

Oxygen Loop 98%

Habitation Space Architecture Planner

Calculate net habitable volume indexes and radiation shielding ratings in our Space Architecture Lab.

Crew Size 4 Crew

Habitable Volume (m³) 120 m³

Volume Ratio 30 m³/crew

Habitability Rating OPTIMAL

Remote Sensing Spectrography

Inspect agricultural fields and moisture indexes with different satellite sensor bands in our Informatics lab.

Satellite Sensor Band

Target Index Alfalfa (Health: 88%)

Resolution Sentinel-2 (10m)

GIS Telescope Field-of-View

Configure optical telescope parameters to evaluate Swath Ground Sample Distance (GSD) resolutions in LEO.

Focal Length (mm)

Satellite Altitude (km) 600 km

Resolution (GSD) 3.6 cm/pixel

Swath Width 15.2 km

Marrakech Ground Station Telemetry

Simulate orbital telemetry downlinks and dish antenna steering controls in our Space Systems Lab.

Telecommand Status

DOWNLINKING

Signal Strength -72 dBm

Received Packets 4096 KB

Radio Link Budget Planner

Configure frequency bands and transmitter power to calculate free space path loss in our Space Systems Lab.

Frequency Band

Orbital Distance (km) 600 km

Path Loss (FSPL) -154.8 dB

Link Status NOMINAL

Star Tracker Attitude Determination

Simulate celestial pattern-matching algorithms to determine satellite 3D attitude coordinates in LEO.

Attitude Roll/Pitch/Yaw -- / -- / --

Match Accuracy UNRESOLVED

Reaction Wheel Desaturation

Monitor fly-wheel momentum saturation and trigger RCS thruster dumps to bleed angular speeds in LEO.

Flywheel Speed (RPM) 5200 RPM

Saturation Level 86.7%

ACS Status NEAR LIMIT

Space Command Encryption

Simulate AES-256 GCM cryptographic handshakes and command key verifications in our Informatics Lab.

Security Level

UPLINK_TERMINAL.log

[SYS] Terminal initialized. Waiting for telecommand input...

Careers & Talent Portal

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