Science & Technology

Optical communications, organ-on-chip biology, crew health monitoring, and deep space network
Artemis II · Mission 1.190 · Science Payloads & Technology Demonstrations

O2O Optical Communications System

Orion carries a 4-inch (100 mm) optical telescope mounted on dual gimbals, enabling laser-based data transmission between the spacecraft and ground stations in California and New Mexico. This is the first crewed deep space test of optical communications, a technology that fundamentally changes how much data we can move from beyond low Earth orbit.

Downlink Rate
260 Mbps
optical laser channel
S-Band Radio
~2 Mbps
conventional RF downlink
Speed Improvement
130x
faster than radio
Wavelength
~1550 nm
telecom IR band
Telescope Aperture
100 mm
4-inch diameter
Gimbal Axes
2
azimuth + elevation

The advantage of optical over radio comes down to beam physics. A laser at ~1550 nm wavelength produces a beam with divergence of approximately 18.9 microradians. A 3-meter S-band dish operating at ~2.2 GHz produces a beam diverging at roughly 55,000 microradians. The optical beam is 2,900 times tighter.

S-Band Radio Footprint
~21,142 km
at lunar distance (384,400 km)
3m dish, ~55 mrad divergence
vs
Optical Laser Footprint
~7.27 km
at lunar distance (384,400 km)
100mm telescope, ~18.9 urad divergence
Why this matters: A tighter beam concentrates energy on the receiver instead of scattering it across thousands of kilometers of empty space. This enables HD video streaming from deep space — not just voice calls and telemetry data. Future missions to Mars and beyond depend on optical links to transmit the science data volumes that radio physically cannot carry at those distances.
Ground Station 1
California
optical ground terminal
Ground Station 2
New Mexico
optical ground terminal

AVATAR — A Virtual Astronaut Tissue Analog Response

AVATAR uses organ-on-chip technology — microfluidic devices containing living human cells arranged to mimic the structure and function of real organs. These millimeter-scale chips simulate physiological responses that would otherwise require exposing actual tissue to deep space conditions over extended periods.

This is the first test of organ-on-chip devices in deep space, beyond the Van Allen radiation belts that partially shield the International Space Station. The ISS orbits within Earth's magnetosphere; Artemis II will carry these devices through the full radiation environment that future lunar surface crews will face.

Technology
Organ-on-Chip
microfluidic tissue analogs
Environment
Deep Space
beyond Van Allen belts
Variables Studied
Radiation + Microgravity
combined exposure effects
Previous Testing
ISS Only
low Earth orbit (LEO)
Why this matters: Before sending crew to the lunar surface on Artemis III, NASA needs data on how deep space radiation and microgravity interact at the cellular level. The combined effect may differ from either stressor alone. AVATAR provides this data without requiring long-duration human exposure — the chips serve as biological proxies for astronaut tissue.

ARCHAR — Artemis Research for Crew Health And Readiness

ARCHAR is a longitudinal study that collects data on crew health before, during, and after the mission. Unlike a single snapshot, this three-phase design captures how the body changes from baseline through deep space exposure and back to recovery, providing a complete picture of the physiological arc of a lunar flyby mission.

Movement Monitoring
Wearable Sensors
actigraphy + motion tracking
Sleep Assessment
Continuous
pre-flight, in-flight, post-flight
Immune Biomarkers
Saliva Samples
immune response indicators
Radiation Exposure
Dosimetry
personal radiation assessment

The study also examines psychological effects of isolation. Four crew members in a relatively small vehicle, farther from Earth than any humans in over fifty years, provide a unique data point for understanding the mental health dimensions of deep space transit. This data feeds directly into crew support planning for longer Artemis III surface missions and eventual Mars expeditions.

Data collection phases: Pre-flight baseline measurements establish each crew member's normal ranges. In-flight data captures changes under actual mission conditions. Post-flight follow-up tracks recovery timeline and any persistent effects. The longitudinal design is what makes this study valuable — single time-point measurements miss the trajectory of change.

CubeSat Secondary Payloads

Four CubeSat secondary payloads from international partners will deploy from the Orion stage adapter ring after trans-lunar injection. These small satellites carry focused experiments that take advantage of the deep space trajectory without adding mass or complexity to the primary mission.

Payload Nation Investigation
TACHELES
Germany (DLR)
Electrical component impact studies in deep space radiation environment. Testing how commercial electronics degrade beyond Earth's magnetosphere.
ATENEA
Argentina (CONAE)
Radiation shielding effectiveness, GPS reception at lunar distance, and deep space communication systems validation.
K-RadCube
South Korea (KASA)
Dosimeter testing and calibration in the deep space radiation environment. Characterizing radiation flux beyond the Van Allen belts.
SWC-1 (Space Weather CubeSat-1)
Saudi Arabia
Space weather measurement and characterization along the cislunar corridor. Solar particle and galactic cosmic ray monitoring.

Deep Space Network (DSN)

NASA's Deep Space Network provides the primary communication link to Orion throughout the mission. Three ground complexes spaced roughly 120 degrees apart in longitude ensure that at least one station can always see the spacecraft, regardless of Earth's rotation.

Goldstone
Barstow, California, USA
70m DSS-14 + 34m BWG antennas
Madrid
Robledo de Chavela, Spain
70m DSS-63 + 34m BWG antennas
Canberra
Tidbinbilla, Australia
70m DSS-43 + 34m BWG antennas
Uplink / Downlink
S-Band + X-Band
radio frequency channels
70m Dish Capability
Deep Space
interplanetary-class antennas
34m BWG Antennas
Beam Waveguide
high-efficiency design
Supplementary Link
O2O Optical
laser comms (see above)

For Artemis II, DSN provides the operational backbone: S-band for voice communication and commands, X-band for higher-rate telemetry. The O2O optical system operates as a supplementary technology demonstration channel, not a primary link. If the laser connection is lost, the mission continues on radio without interruption.

Watch DSN live: NASA's DSN Now interface at eyes.nasa.gov/dsn/dsn.html shows real-time antenna pointing and data rates for every active spacecraft. During Artemis II, you can see which dishes are tracking Orion and the current uplink/downlink status.

What Makes This Different from Artemis I

Artemis I (November 2022) was an uncrewed test flight that validated the SLS rocket and Orion spacecraft systems. Artemis II adds crew, science, and new technology to transform a vehicle test into a deep space expedition.

  • Crew aboard
    Four astronauts (3 NASA + 1 CSA) versus uncrewed Artemis I. First humans beyond low Earth orbit since Apollo 17 in December 1972.
  • Life support systems active and tested
    Environmental Control and Life Support System (ECLSS) operating under real crew load. Artemis I carried sensors only, no active life support demand.
  • Optical communications first
    O2O laser terminal providing 260 Mbps downlink. Artemis I used radio only. This is the first crewed deep space optical link ever attempted.
  • Science payloads
    AVATAR organ-on-chip and ARCHAR crew health studies. Artemis I carried technology demonstrations but no biological or crew health investigations.
  • Modified reentry trajectory
    Steeper direct reentry rather than the skip reentry profile used on Artemis I. Different thermal and G-loading profile on the heat shield. The skip entry on Artemis I bounced off the upper atmosphere to reduce peak heating; Artemis II enters more directly.
  • International CubeSat payloads
    Four secondary payloads from Germany (DLR), Argentina (CONAE), South Korea (KASA), and Saudi Arabia. Deep space radiation and technology experiments.
Sources: NASA Artemis II Press Kit · NASA O2O Optical Communications · NASA AVATAR Investigation · NASA ARCHAR Study · JPL Deep Space Network · NASA CubeSat Partners