Image of University of Toronto Institute for Aerospace Studies Space Flight Lab - XPOD DUO - Cubesat Deployer on the satsearch marketplace

Key highlights

The XPOD Separation System was developed for nanosatellites and small microsatellites. The XPOD is an enclosed "jack-in-the-box" container for separating nanosatellites from virtually any launch vehicle. Various models are available, including models compatible with the CalPoly CubeSat standard. Once a deployment signal is received from the launch vehicle, a power supply inside the XPOD activates a release mechanism causing a door to open and the spacecraft to be ejected. The XPOD implements a single-failure fail-operational design, and is customizable for spacecraft up to 16kg with arbitrary dimensions. Also available are semi-enclosed (or "open concept") designs that accommodate fixed appendages. XPODs come in various standard models – the XPOD Single, XPOD Triple and XPOD GNB. Specifications are subject to change. Unit is delivered with functional testing only. Environmental acceptance is not performed unless negotiated with the customer.

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Last updated: 2021-03-11

Image of University of Toronto Institute for Aerospace Studies Space Flight Lab - XPOD DUO - Cubesat Deployer on the satsearch marketplace

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Technical specs

mass
10 kg
width
47 cm
length
47 cm
height
52 cm
operating temperature
-35 to 65 C

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