Failure reason: Vehicle lost attitude control after first stage motor nozzle thrust vector control (TVC) failure at T+80s.

Second flight of the KAIROS launch vehicle. 5 satellites for testing various technologies will be on board: * TATARA-1 * PARUS-T1A * SC-Sat1 * ISHIKI

Mission type: Test Flight · Orbit: Sun-Synchronous Orbit

Rocket: KAIROS · Provider: Space One