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IOD on a dedicated CubeSat.

One payload per mission: yours.

With the render focused, the arrow keys rotate it.

  • 1/3 U · 1Uof payload, by format
  • 1customer per satellite
  • LEOorbit per rideshare [PENDING]
  • Raw + processedcustomer-owned dataset, no licence reserved
1U (1/3 U payload) and 3U (1U payload over a 2U bus). Render; Earth: NASA Blue Marble from 500 km. Envelopes and dimensions

1/3 U of payload on a 1U bus, or 1U on a 3U bus, in LEO. Operations driven by your test plan, platform telemetry on the same time base as your DUT, and at close-out a raw and processed dataset, a performance report and a flight certificate.

The bus is operated around your test plan.

No power, storage or link windows shared with other payloads.

Synchronised instrumentation

Your DUT channels plus per-line V/I, temperatures, attitude, position and time from the platform, on a common time base.

Your own operating profile

Power-ups, duty cycle, voltage and temperature sweeps and logging cadence, within the resources in the ICD.

Several DUTs per slot

Parts from the same family or lot in the same payload slot, with power and test time split agreed before flight.

Ground correlation

SEE, SEL, thermal drift and TID degradation measured in flight against your beam and TVAC campaigns.

Applications by segment

Two formats. One customer in each.

Pick the payload slot your DUT needs.

CubeSat 1U

Entry format

37.8 mm

nominal payload height

Payload
1/3 U
Envelope
100 × 100 × 37.8 mm
Bus
2/3 U · body-mounted cells

CubeSat 3U

For larger or higher-power DUTs

113.5 mm

nominal payload height

Payload
1U
Envelope
100 × 100 × 113.5 mm
Bus
2U · deployable panels

Parameter-by-parameter comparison

What gets flown.

By segment, the kind of DUT that fits the slot.

  • Communications constellations

    RF front-ends, SDRs, power conversion and baseband processing.

  • Earth observation

    Front-end electronics, on-board compression and processing, mass memory.

  • On-board computing

    COTS FPGAs, SoCs, GPUs and inference accelerators; DDR and flash.

  • Power

    DC-DC and POL, GaN and SiC stages, distribution, protection and BMS.

  • Navigation and timing

    GNSS receivers, oscillators and time references.

  • COTS and automotive grade

    Industrial and AEC-Q parts heading for a space variant.

What gets flown and characterised in each segment

From signature to data, in four phases.

Each one closes with a reviewable deliverable.

  1. 1

    Kick-off and integration

    ICD frozen, flight model integrated and system-level environmental campaign.

    DeliverableSigned ICD + environmental test report

  2. 2

    Licensing and launch

    Operator, frequencies, export control and a rideshare slot.

    DeliverableLicences in force + manifest confirmation

  3. 3

    In-orbit operations

    Commissioning and the test campaign for your payload, orbit by orbit. Watch it live

    DeliverableOperations reports + preliminary telemetry

  4. 4

    Data and certificate

    Raw and processed dataset, performance report and flight certificate.

    DeliverableData + performance report + flight certificate

Phases, deliverables and inputs from your team

Send us your DUT profile.

Envelope, mass, power profile, interfaces and test plan. We reply with a fit analysis against the ICD and the open technical questions.