
Origin Antares® Incorp's Single Piece Bell Shaped Convergent Divergent Nozzle. This nozzle is compatible with 1U, 2U, and 3U CubeSat configurations and can be modularly adapted for higher units up to 6U, ensuring optimal thrust-to-mass ratio for satellite propulsion in nanosatellite and microsatellite applications, a key aspect of innovative space technology.

Origin Antares® Incorp's Single Piece Multi-Staged Advanced Hybrid Cubesat Propulsion Nozzle (Series-II) This nozzle is compatible with 1U, 2U, and 3U CubeSat configurations and can be modularly adapted for higher units up to 6U, ensuring optimal 1U & 2U CubeSats: Single nozzle integration for micro-thrust vectoring.

Origin Antares® Incorp's ORION - Series I
Designed and Manufactured in-house at Origin Antares® Incorp., with precision, modularity, and long duration orbital reliability, this solar panel assembly forms the primary electrical power source for CubeSats operating in Below Low Earth Orbit (BLEO), Low Earth Orbit (LEO), Sun Synchronous Orbit (SSO), and extended mission profiles.

Origin Antares® Incorp's OA - 40X
Designed and Manufactured in-house at Origin Antares® Incorp., with precision, modularity, and long duration orbital reliability, this nozzle for CubeSats operating in Below Low Earth Orbit (BLEO), Low Earth Orbit (LEO), Sun Synchronous Orbit (SSO), and extended mission profiles.

Origin Antares® Incorp's PEGASUS
Series-1 On-Board Computer.
Designed and Manufactured in-house at Origin Antares® Incorp., with precision & modularity. PEGASUS is designed for seamless integration across:
Mission Applications:
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