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RCM Canadian SmallSat bus

RCM Canadian SmallSat bus is the platform module used for the three identical RCM spacecraft.[1] It provides attitude and orbit control, power generation and storage, payload command handling, telemetry, thermal control, and primary support structure.[1] The spacecraft mass is 1,400 kg, peak power is below 1,600 W, average power is below 220 W, and bus dimensions are 3.6 m x 1.1 m.[1][2]

Operator pricing

Pricing not publicly listed by operator

Supply chain position

Sources
Cite https://eo-atlas.org/products/bus/rcm-smallsat-bus Markdown twin → Field definitions → Suggest a correction →
How to cite this page

Plain text

RCM Canadian SmallSat bus. EO-Atlas, SpectraWorks B.V. https://eo-atlas.org/products/bus/rcm-smallsat-bus (CC BY 4.0)

BibTeX

@misc{eoatlas:products:bus:rcm-smallsat-bus,
  title = {RCM Canadian SmallSat bus},
  author = {{EO-Atlas}},
  publisher = {SpectraWorks B.V.},
  note = {CC BY 4.0},
  url = {https://eo-atlas.org/products/bus/rcm-smallsat-bus}
}