SpinLaunch can help to choose additional needed flight hardware such as the OBC, propulsion and communication from their preferred supplier list of components. The standard bus configuration will include the following components SP-20, EPS-20, BP-20, RW-20, 3X MT-20, in addition to various sensors. The bus is configured with ~100W of available solar array with up to 6U of payload volume and 4kg payload mass pending performance requirements. Our Space Systems engineering team will offer additional design support for new space customers as well as operational services for those that need support managing their satellites in orbit. ![]() The buses unique feature includes a reinforced support structure on the chassis that enables qualification on the SpinLaunch launch system. read more S-20 is compatible with NASA GEVS and SpinLaunch's mass accelerator environments, including the shock, vibe, lateral-g loads, and thermal requirements. ![]() The bus is also ideally suited for prototyping, technology development, and experimentation such as scientific research, space systems R&D, flight heritage qualification or Earth Observation (EO). ![]() S-20 the ideal size mix for a range of applications, including LEO constellations for providing services covering Automatic Dependent Surveillance-Broadcast (ADS-B), Internet of Things (IoT), Machine to Machine communications (M2M), Automated Identification Services (AIS) or Emergency communications platforms. The SpinLaunch S-20 is a 12U, 20 kg bus designed for rapid development and experimentation in space.
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