Exolaunch and INNOSPACE have signed a Strategic Partnership Agreement (SPA) to collaborate on launch integration services and broaden access to orbit for global satellite customers.
Through this agreement, Exolaunch and INNOSPACE will work together on launch manifest planning, mission management and payload integration for upcoming commercial launch campaigns. Exolaunch will provide its flight-proven separation systems for cubesats and microsatellites (smallsats), with its hardware positioned as the deployment solution for INNOSPACE customers across dedicated and rideshare missions.
The partnership also includes the use of Exolaunch’s EXOtube, a modular and scalable launch platform designed to optimize multi-payload configurations, increase mission flexibility, and enhance vehicle utilization. The teams will further collaborate on launch campaign planning, system integration, and on-site execution support.
Exolaunch’s mission heritage includes more than 530 satellites deployed across 36 missions, with customers ranging from leading commercial operators and startups to space agencies, leading universities and research institutions. INNOSPACE is currently ramping up launch services with the HANBIT series powered by hybrid and methane engines.
We’re proud to partner and formalize our work with INNOSPACE to bring new flexibility and reliability to global customers seeking access to orbit,” said Jeanne Allarie, Chief Commercial and Marketing Officer at Exolaunch. “Our separation hardware and mission services are designed to scale across launch vehicle platforms, and this partnership supports our commitment to enabling global launch diversity. We look forward to launching with the HANBIT series in the near future.”
Exolaunch’s hardware heritage and integration experience make them an ideal partner as we expand INNOSPACE’s launch cadence and international customer base,” said Soojong Kim, founder and CEO of INNOSPACE. “This collaboration will help us deliver smooth, safe, and efficient launch campaigns for a growing range of payload configurations.”
