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Quadro Arrow

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Four-point microsatellite separation system tailored to the Arrow 150 satellite interface and satellites with masses up to 250 kg.

Quadro Arrow is an Exolaunch four-point microsatellite separation system for orbital deployment hardware, tailored to the Arrow 150 satellite interface.[1][2] The Arrow 150 configuration has a combined stowed mass of 8.4 kg, including 1.58 kg for the four S-adapter points and 6.82 kg for the L-adapter.[1] The interface uses 16 M8 fasteners, four hold-down and release points, mechanically synchronized release, and pusher-arm deployment.[1] Maximum load per release mechanism is specified as plus or minus 75 kN axial, plus or minus 20 kN shear, and 1150 Nm bending.[1] The nominal signal is 24 VDC for 0.5 s, and average separation time is 0.1 s.[1] Payload limits include up to 250 kg for Arrow 150, up to 300 kg, and broader 150 kg to 800 kg suitability for the product family.[2][3][1] Separation velocity is tailored with four springs using brown, black, and green energy choices of 1.1 J, 2.2 J, and 3.7 J.[1] Quadro Arrow flight heritage starts in Q1 2025, with Transporter-13 and Transporter-14 included as 2025 mission heritage for the product.[2][3]

Sources
Cite https://eo-atlas.org/launch_services/quadro-arrow Markdown twin → Field definitions → Suggest a correction →
How to cite this page

Plain text

Quadro Arrow. EO-Atlas, SpectraWorks B.V. https://eo-atlas.org/launch_services/quadro-arrow (CC BY 4.0)

BibTeX

@misc{eoatlas:launch_services:quadro-arrow,
  title = {Quadro Arrow},
  author = {{EO-Atlas}},
  publisher = {SpectraWorks B.V.},
  note = {CC BY 4.0},
  url = {https://eo-atlas.org/launch_services/quadro-arrow}
}